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Fiat G.50 In Finnish Service 

Finland, , , , , , , , , , , ,

Finnish flag Finland (1940-1944)
 Fighter – Number operated: 35

In late 1939, the rapid expansion of the Soviet Union in Eastern Europe caused great alarm in Finland. As a politically isolated nation with limited funds, Finland struggled to equip its military for a potential war with the Soviets. Despite the challenges they faced, they achieved some limited success in finding the equipment they needed. While the Finnish armed forces lacked for many modern weapons, they possessed a small number of advanced fighter aircraft, though not enough in the face of a Soviet invasion. To address this, they approached the Kingdom of Italy and acquired 35 Fiat G.50 Freccia fighters. While the G.50 was not an exceptional fighter in terms of overall performance, it was sufficient for the Finnish Air Forces and remained in frontline service until 1944.

The Fiat F.50 in Finnish service. Source: https://en.wikipedia.org/wiki/Fiat_G.50_Freccia

Finland’s Early Struggle to Survive 

Following the collapse of the Russian Empire, and the subsequent Civil War, Finland emerged as an independent state. While it did not have great relations with the neighboring Soviet Union, Finland’s first two decades of independent existence proved to be mostly peaceful. This changed drastically on 27th August 1939, when a secret meeting between German Foreign Minister Joachim von Ribbentrop and Soviet Foreign Minister Vyacheslav Molotov resulted in the Molotov-Ribbentrop Pact. This non-aggression pact had secret protocols dividing Eastern Europe into spheres of influence, which directly affected Finland. As part of the agreement,  Germany agreed to let the Soviets occupy former territories that had belonged to the Russian Empire. By September, the Soviets were in the process of occupying the Baltic states under the pretext of defending against a possible German attack. These countries were mostly too small to offer any real resistance to the Soviet demands.

Fearing a potential war with the rapidly expanding Soviet Union, Finnish military officials sought to acquire as many weapons and as much material as possible, including aircraft. As part of this, a delegation was dispatched to Italy. This delegation visited Turin in 1939, where new G.50 fighter was being tested. The Finnish representatives were impressed with the aircraft’s performance and promptly placed an order for 35 brand-new G.50s.

In November 1939, while testing the G.50’s capabilities, Finnish pilot Tapani Harmaja took a sharp dive from an altitude of over 3.5 km, reaching a remarkable speed of 830 km/h during his descent. Ironically, this was the highest speed achieved by any Italian aircraft up to that date.

Purchasing the 35 aircraft was the easy part; transporting them to Finland proved to be a much more challenging task. By then, the Second World War had already begun in Europe with the German invasion of Poland. With limited options, the aircraft were disassembled into smaller parts and transported by train to northern Germany. From there, they were loaded onto ships bound for neutral Sweden. Due to various delays, the first aircraft was not fully assembled until mid-December 1939, and the last of the 35 ordered fighters did not arrive in Finland until June 1940.

In the hope of acquiring more modern fighters Finland purchased 35 new Fiat G.50 fighters from Italy. Source:  airpages.ru

The Fiat G.50, a Brief History

During the 1930s, the Italian Ministry of Aviation (Ministero dell’aeronautica) was interested in adopting a new, all-metal monoplane fighter and ground-attack aircraft for the Italian Air Force (Regia Aeronautica). In April of 1935, engineer Giuseppe Gabrielli began working on a new low-wing, all-metal aircraft designated G.50. On 28th September 1935, Gabrielli submitted his project to the Ministry of Aviation. Military officials were impressed by the design and ordered him to proceed with his work. As Fiat’s production capacities were overburdened, work on this new project was instead moved to the Costruzioni Meccaniche Aeronautiche (CMASA) works at the Marina di Pisa, which had been a part of Fiat since 1931. By 1936, Giuseppe Gabrielli had completed his last drawings and the list of needed materials and equipment in.

The prototype was completed in early 1937 and was transported to the city of Turin for further testing. The prototype, under registration number MM 334, made its first test flight on 26 February 1937. Once accepted for service, the Fiat G.50 would become the first Italian all-metal monoplane fighter. Between 1938 to 1943, some 774 to 791 G. 50s would be built. These saw combat service starting from 1938 in the Spanish Civil War, until 1943 when the few surviving aircraft were reassigned to secondary roles.

G.50s flying in formation with a German Bf-110, possibly during the Battle of Britain Source; Wikipedia

In Finnish Service

While the G.50 proved to be a fairly modern fighter, they arrived too late and in too few numbers to have any real impact in the Winter War. The Soviet Union then demanded territorial concessions from Finland, particularly the lease of the Karelian Isthmus and other areas near Leningrad. The Finns were reluctant to comply, leading to unsuccessful negotiations. When diplomatic negotiations failed, the Soviet Union launched a military offensive against Finland on 30 November 1939. Despite being outnumbered and outgunned, the Finnish military, with their knowledge of the terrain and effective guerrilla tactics, inflicted significant casualties on the Soviet forces. The harsh winter conditions also worked to Finland’s advantage.

With the gradual arrival of the G.50, these aircraft were assigned to the  Lentolaivue 26, or shortened, LeLv 26 (REng. 26th Fighter Wing). This unit was based at Haukkajärvi. Although the G.50s arrived late, they still saw significant action. Between February and March 1940, Finnish pilots flying these aircraft managed to shoot down 11 Soviet planes, losing only one of their own.

There is some disagreement among sources and authors regarding the use of the Fiat G.50 during the Winter War. According to P. Vergnano (Fiat G.50), the aircraft was deployed in this conflict. However, other authors, such as G. Cattaneo (The Fiat G.50), state that 14 aircraft reached Finland by February 1940, and were assigned to the 26th Fighter Wing, but they did not see action until after March 1940. D. Monday (The Hamlyn Concise Guide to Axis Aircraft of World War II), simply mentions that they arrived too late to participate in the Winter War.

Despite the Finns’ valiant resistance, they were eventually forced into peace negotiations with the Soviets. The war concluded with the signing of the Treaty of Moscow on 12th March 1940. Though brief, the conflict was costly for both sides, and Finland was compelled to cede roughly 10% of its territory to the Soviet Union, including the Karelian Isthmus. Finnish military officials, however, recognized the need to prepare for future conflicts.

Camouflage And Marking

Initially, the G.50 would use camouflage of Italian origin, featuring a combination of green, brown, and sand backgrounds. In 1941, at the insistence of the Germans, the original Italian camouflage colors would remain unchanged for the Finnish planes. However, the Italian paint was prone to peeling, so ground crews used whatever was available to repair the damage. After 1942, most aircraft were repainted with Finnish camouflage colors, such as black, olive green, and light blue.

The first aircraft that arrived in Finland was designated with the code SA-1. This was later changed to FA-1 (up to FA-35) in late January 1940, with the capital ‘F’ standing for Fiat.

The standard Finnish Insignia was a Hakaristi cross, commonly referred to as a swastika, on either side of the fuselage. The Finnish Hakaristi is often conflated with the swastika used by Nazi Germany, however, the Hakaristi was not derived from the German swastika and had been used in Finland since 1918, drawing from much older cultural use. The Hakaristi markings were blue with a round shape and a white background.

Additionally, commanding fighters often had large numbers painted on their tails. The first squadron fighter leader’s aircraft had a light blue number, followed by a black number with yellow trim for the second, and a yellow number for the third. After 1942, the light blue color was replaced by a simpler white.

The first G.50 (initially marked as SA-1 later changed to FA-1) reached Finland. This aircraft used for initial testing and crew training. Source: en.topwar.ru
The standard Finnish roundel was a Hakaristi cross which as painted on the fuselage sides. Source: ww2aircraft.net
The first squadron fighter leader’s aircraft had a light blue number, followed by a black number with yellow trim for the second, and a yellow number for the third. After 1942, the light blue color was replaced by a simpler white. Source: ww2aircraft.net

Continuation War 

While not fully aligned with Nazi Germany, Finland did allow the Wehrmacht access to Northern Finland. Finland later signed the Anti-Comintern Pact, which was initially an anti-communist pact between Germany and Japan, with other minor nations signing throughout the war. Prior to this, relations had already been previously established, which was convenient for both nations, as Germany could stage their military in Lapland, and other areas of Finland, for Operation Barbarossa. In turn, Finland would be granted the military assistance they needed. However, this ended all support, both material and political, from the Western Allies. On the 22nd of June 1941, Germany’s invasion of the Soviet Union began, assisted by some Finnish forces. Three days later, the Soviets staged air raids against nearby Finnish cities, thus beginning the Continuation War. Finland never sought to gain any additional territory from the conflict, only to regain control of what was initially lost during the Winter War.

Just before the outbreak of the Continuation War, the Finns observed that the newly arrived G.50 aircraft were somewhat ill-suited for operating in the harsh Northern climate. This was not entirely unexpected, as the aircraft had been designed in Italy, a much warmer region, and the designers had not anticipated the need for the G.50 to function in colder parts of the world. In response, the Finnish Army attempted to modify the G.50 to enhance its effectiveness in these conditions.

The G.50s that the Finns received were from the first production series, which featured enclosed cockpits. This design element was not well received by Finnish pilots, leading to the replacement of the enclosed cockpits with open ones. Additionally, the aircraft’s variable-pitch propeller mechanism had a tendency to freeze in low temperatures, risking critical component failure. To address this issue, the Finns turned to Sweden for assistance, importing Swedish propeller spinners that were better suited for cold climates. These spinners were originally used on Swedish-imported CR.42 and J11 biplanes, which had faced similar issues.

Further modifications included replacing the original G.50 fins and rudders with improved versions. Finnish engineers also experimented with the installation of landing skis for use in snowy conditions.

To avoid freezing of some parts of the propellers, Finish engineers added a new Swedish propeller spinner, as seen here. Source: P. Verganano Fiat G.50

When the war resumed, the 26th Fighter Wing, stationed at an airfield near Utti, was tasked with defending the area around Lake Ladoga, where they saw the bulk of their action. From the outset, Finnish pilots operating the G.50 achieved remarkable success. On the first day of the conflict, the six G.50s managed to shoot down ten Soviet bombers without suffering any losses. One pilot, Oiva Tuominen, alone shot down four of these bombers within a matter of minutes. Tuominen would go on to become one of Finland’s top fighter aces, credited with a total of 23 air victories (though some sources claim 33 or even 43), with around 15 of these achieved while flying the G.50. For his service, he was awarded the Mannerheim Cross, Finland’s highest military decoration at the time. In 1941, following the German invasion, the number of Soviet aircraft on this front sharply declined.

In late August 1941, they successfully shot down nine Soviet fighters. By the end of the war, pilots of the 26th Fighter Wing had achieved approximately 88 air victories, with the loss of 11 G.50 aircraft. Of these, only two were downed by Soviet fighters, one was lost to anti-aircraft fire, and eight were lost due to accidents or mechanical failures.

By 1943, the introduction of newer Soviet fighter models and better-trained pilots forced the Finnish Air Force primarily into a defensive role. At this point, the G.50 was clearly obsolete as a frontline fighter, but due to a lack of alternatives, it remained in service until 1944. After May 1944, the surviving aircraft were withdrawn and relegated to secondary roles, such as training. However, by the end of the war, several operational G.50 fighters remained in use, with some continuing to serve until 1947.

Technical characteristics

The G.50 was a single-seat, low-wing, all-metal fighter plane. The fuselage was made from four angular longerons. The wing construction consisted of a center section which was made of a steel tube connected to the lower fuselage and two metal spars connected with ribs. The fuselage, wing, and tail were covered with duralumin sheets. The only fabric-covered parts of the aircraft were the movable control surfaces in the wings and the tail. The G.50 was powered by the 840 hp (626 kW) Fiat A 74 RC 38, a 14-cylinder radial piston engine, which drove an all-metal three-blade propeller produced by Fiat.

The G.50 was equipped, like most modern aircraft of the time, with inward retracting landing gear, but the rear tail wheel was fixed. In later improved versions, the rear tail wheel was changed to a retractable type as well.

The armament consisted of two forward-firing 12.7mm Breda-SAFAT heavy machine guns, with 150 rounds of ammunition for each gun. The guns were placed behind the upper engine cowl and were synchronized in order not to damage the propeller.

In Finnish service, these aircraft received several modifications as mentioned earlier. This included an open pilot cockpit, enlarged tail control surfaces, and propeller spinners which protected the variable pitch mechanism from the cold climate.

The Finnish version could be easily identified by the open cockpit and the use of an engine spinner, Source: www.militaryimages.net

Conclusion

The acquisition of the Fiat G.50 provided Finnish pilots with a more modern fighter aircraft. While the design was not exceptional from the start, the Finns managed to put it to good use, achieving relatively good success against the Soviet Air Force. The G.50 remained in service well into the later stages of the war.

Specification G.50 Fighter
Wingspan 35 ft 11 in / 10.9 m
Length 26 ft  3 in / 8 m
Height 10 ft 7 in / 3.28 m
Wing Area 196.5 ft² / 18.25 m²
Engine One 840 hp (626 kW) Fiat A.74 RC.38, 14 cylinder radial piston
Empty Weight 4,353 lbs / 1,975 kg
Maximum Takeoff Weight 5,324 lbs / 2,415 kg
Fuel Capacity 316 l
Maximum Speed 292 mph / 470 km/h
Range 267 mi / 445 km
Maximum Service Ceiling 35,100 ft (10,700 m)
Climb speed Climb to 19,700 ft (6,000 m) in 7 minutes and 30 seconds
Crew One pilot
Armament
  • Two 12.7 mm Breda-SAFAT heavy machine guns

Illustration

Credits

  • Article written by Marko P.
  • Edited by  Henry H.
  • Illustration by Haryo Panji

Sources 

  • V. Nenye (2016) Finland At War  The Continuation And Lapland Wars 1941-45, Osprey Publishing
  • V. Nenye (2015) Finland At War The Winter War, Osprey Publishing
  • P. Jowett and B. Snodgrass (2006) Finland At War 1939-45, Osprey Publishing
  • D. Nesic (2008)  Naoružanje Drugog Svetsko Rata-Italija. Beograd
  • C. Shores (1979) Regia Aeronautica Vol. I, Signal publication.
  • D. Monday (2006) The Hamlyn Concise Guide To Axis Aircraft OF World War II, Bounty Books.
  • V. Nenye (2016) Finland At War The Continuation And Lapland Wars 1941-45, Osprey Publishing
  • V. Nenye (2015) Finland At War The Winter War, Osprey Publishing
  • P. Jowett and B. Snodgrass (2006) Finland At War 1939-45, Osprey Publishing
  • P. Verganano (1997)  Fiat G.50, La Bancarella Aeronautica
  • A, Brioschi (2000) I Colori Del Fiat G.50, La Bancarella Aeronautica
  • G. Cattaneo The Fiat G.50, Profile Publication

 

Re.2000 (J20) In Swedish Service

Sweden, Uncategorized, WW2, , , , , , ,

sweden flag Sweden (1941)
Fighter – 60 Aircraft

To protect their airspace as the Second World war ravaged Europe, Sweden wanted to acquire more modern fighters. Initially, they purchased American fighters, but the few they could order  were insufficient and would be soon out of date. Luckily for Sweden,  Italy was in short supply of vital metal ore, so it was that the Swedish Air Force managed to acquire 60 Re.2000 fighters. These were immediately put to service and proved to be the best fighters that Sweden had in its inventory during the war.

J20 (Re.2000) in Swedish service. Source: www.destinationsjourney.com

History

As the war in Europe broke out in 1939, Sweden tried to use its geopolitical and geographic position to remain neutral. Despite its neutral position, it still needed to acquire weapons and other pieces of military equipment to protect its border in case of any potential attack. Just as the war in Europe started,  Sweden’s military officials purchased 120 P-35 Seversky fighters from the US to strengthen its air force. The first contingent of 60 aircraft reached Sweden in early 1940. The second group never reached Sweden, as the US Government canceled this agreement.

Despite ordering 120 P-35 Seversky fighters only half that number ever reached Sweden. Source: comandosupremo.com

The Swedish Armed Forces, not wanting to be left defenseless against an enemy air force, instead approached the Italians. Luckily for them, the Italians had developed and produced the Re.2000 which was essentially an improved copy of the US P-35. The Swedish government requested the purchase of 60 aircraft of this type. The official agreement was signed on the 28th of November 1940. As payment, Sweden agreed to give the Italians vital ore resources such as chrome and nickel.

Through Italy, Sweden managed to acquire 60 Re.2000 fighter aircraft in 1941. Source:www.destinationsjourney.com

Re.2000 Brief Development History 

In 1938, the development of the Re.2000 by Reggiane began at the request of the Italian Aviation Ministry. The Italian Air Force at that time wanted to introduce more modern, low-wing fighters. By then, several different fighter designs were in various states of development. Reggiane formed a team of engineers with the aim of creating such a fighter, led by the Technical Director Antonio Alessio, and Engineer Roberto Longhi. Due to a lack of time to design an aircraft from the ground up, a solution was made to utilize some elements of the design of the US Seversky P-35. The main reason why the Re.2000 was influenced by this US design was Roberto Longhi. He had spent some time working in the aviation industry in America before returning to Italy in 1936. While the two planes look very similar, there were some differences, like the cockpit, and landing gear. Due to the lack of interest of the Italian Air Force Officials, fewer than 170 aircraft of this type would be produced. Most were exported, and only small quantities of this fighter were ever operated by the Italian Air Force.

 

Italian Re.2000 fighter. Source: www.warbirdphotographs

In Swedish service 

The first Re.2000 reached Sweden in 1941. It was disassembled and then transported by rail through Germany and finally to Sweden. Once there, it was transported to the Swedish Air Force central workshop at Malment to be reassembled, after which the first trial and evaluation flights were carried out in September 1941. Once all 60 arrived, these were allocated to the F 10 Kung. Skanska Flyglottiljen (Eng. Fighter wing) unit. Their primary base of operation was the airfields at Bulltofta and Rinkaby. In Swedish Service, the Re.2000s were renamed to J20. The ‘J’ stands for Jacktplan, meaning a fighter. These received serial numbers from 2301 to 2360. The last two digits of these numbers were painted (in white color) on the aircraft tails and engine.

In general, the overall flight performance of the J20 was deemed sufficient. Its greatest downside was its poor mechanical reliability, and the difficulty in maintaining its engine. The Italians never tested the Re.2000’s performance in a cold climate, as it was intended for service in the Mediterranean. Because of this, the Swedish maintenance crews had to find out the hard way that the aircraft was simply not suited for the cold climate in the North. Trouble starting the engine in cold weather would prove a common, and frustrating exercise.

The J20 mainly saw service in the role of the interceptor. Their job was to intercept any aircraft that came near Sweden’s airspace. These were in the majority of cases, damaged Allied aircraft that were returning from bombing raids in  Germany. On rare occasions, some German aircraft would lose their way and be intercepted by the J20. The interception operations were not intended to engage incoming aircraft but to simply escort them to the Bulltofta airfield, where the plane and its crew would be interred.

During the war, some 16 J20s were lost in various accidents but only one was shot down in combat. During a routine patrol on the 3rd of April 1945, a J20 piloted by Erik Nordlund spotted a German Do 24 aircraft that was flying near Nahobukten. As the J20 approached the German plane it was hit by 2 cm cannon rounds. While the pilot disengaged and tried to fly back, the engine exploded in midair, destroying the aircraft and killing the pilot. The J20s that survived the war remained in the inventory of the Sweden Air Force up to 1955 before being finally removed from service.

Besides their national marking, the Swedish added two large two-digit designations to the J20. These large numbers were painted in white color. Source: www.destinationsjourney.com

Surviving aircrafts

Most were either lost or scrapped, and today, only one J20 is preserved. It is currently exhibited at the Swedish Air Force Museum at Linkoping.

The preserved Swedish J20 fighter (serial number 2340). Source: plasticfantastique.com

Technical characteristics

The Re.2000 was designed as a low-wing, mixed-construction, single-seat fighter plane. The fuselage consisted of a round frame covered with a metal sheet held in place using flush-riveting. The Re.2000 wings had a semi-elliptical design, with five spars covered with stressed skin. The central part of the wing held two integral fuel tanks. The tail section had a metal construction with the controls covered with fabric.

The landing gear system was unusual. When it retracted, it rotated 90° (a copy from the Curtiss model) before it entered the wheel bays. For better landing handling, the landing gear was provided with hydraulic shock absorbers and pneumatic brakes. The smaller rear wheel was also retractable and could be steered.

The Re.2000 engine was the Piaggio P.XI R.C.40 14-cylinder air-cooled radial engine, providing 985 hp, equipped with a three-blade variable pitch propeller made by Piaggio.

The cockpit canopy opened to the rear and the pilot had a good overall view of the surroundings. For pilot protection, a 8 mm (0.3 in) thick armor plate was placed behind the seat.

The Re.2000 possessed weak offensive capabilities, as it was armed with only two Breda-Safat 12.7 mm (0.5 in) heavy machine guns. The machine guns were installed in the forward front fuselage and fired through the propeller arc. For each machine gun, 300 ammunition rounds were provided. The Re.2000 also had two small bomb bays placed in each central wing section. Each bomb bay had a payload of twenty-two 2 kg (4.4 lb) anti-personnel or incendiary bombs.

Conclusion

The J20 was the best fighter in service within the Swedish Air Force. It was noted that during its service it possessed good overall flight characteristics. There were several issues with its maintenance, but this was mainly attributed to the cold Scandinavian Climate.  In conclusion, while not the best fighter of the Second World War, for the country as Sweden it was more than enough to protect its airspace.

Re.2000 Specifications  
Wingspans 11 m  / 36 ft
Length 8 m  / 26 ft 5 in
Height 3.15 m  / 10 ft 4 in
Wing Area 20.4 m² /  220 ft²
Engine One Piaggio P.XI RC.40 985 hp
Empty Weight 2,460 kg   / 5,424  lbs
Maximum Takeoff Weight 3,240 kg   / 7,140  lbs
Climb Rate to 6 km 6 minutes 10 seconds
Maximum Speed 515 km/h  / 320 mph
Cruising speed 450 km/h / 280 mph
Range 840 km / 520 miles
Maximum Service Ceiling 11,500 m /  34,450 ft
Crew 1 pilot
Armament
  • Two 0.5 in (12.7 mm) heavy machine guns
  • 44 kg bombs
Swedish J 20 (Re.2000) with 42 marking number

Credits:

  • Written by Marko P.
  • Edited by Henry H.
  • Illustration by Pavel

Source:

  • G. Punka (2001) Reggiane Fighters in Action, Squadron/signal publication
  • D. Nešić  (2008)  Naoružanje Drugog Svetsko Rata-Italija. Beograd.
  • D. Monday (2006) The Hamlyn Concise Guide To Axis Aircraft OF World War II, Bounty Books
  • M. D. Terlizzi. (2002). Reggiane Re 2000: Falco, Heja, J.20. IBN
  • G. Cattaneo () The Reggiane Re.2000, Profile Publication

 

Saab 340 AEWC

Modern Aviation, Sweden Modern, , ,

sweden flag Sweden (1997)
 Airborne Early Warning & Control (AEWC) Aircraft- 12 Built

The Saab 340B AEW&C and the Saab 2000 AEW&C are airborne early warning and control (AEW&C) airplanes that were developed from the basic Saab 340B airplane, a twin-engine turboprop regional airliner developed and built in partnership with the now defunct American aircraft manufacturer Fairchild Aircraft .  The model was named “Metro III” when manufactured by Fairchild Aircraft. The Saab 2000 AEW&C is based upon the Saab 2000 airliner,it being a variant of the basic Saab 340B model. These airborne radar models came from the inventiveness of the Flygvapnet, as the idea of fitting the basic transport model already in service emerged considering the gaps the Flygvapnet had regarding the type of air asset. This paid off as the Nordic nation is now equipped with an airborne and air control (flying) system that provides a very valuable tool for the Flygvapnet to monitor the Swedish skies and even abroad, as the post-Cold War era meant new missions beyond national defence for the Swedish Armed Forces in general. The basic 340B  version was, despite its initial non-military use, a display of technological advancement with advanced avionics and a product of the company’s desire to revive its interests in the civil market after the not entirely successful Saab Scandia 90, in the 50’s.

The Saab 340B AEW&C (Saab 340B) is a twin-engine turboprop medium size airliner, capable of carrying more than 30 passengers and with a conventional design, mainly for short-range regional flights. The main airframe is cylindrical, with the wings placed near the middle section of the airplane and of trapezoid and thin configuration. The nose is not rounded being rather sloped downwards, and the wings and horizontal control surfaces being angled upwards. The engines are not beneath the wings, as the configuration is that of a low-wing airplane; instead, they are placed above the wings and logically enrooted in them. The Saab 2000 differs from the basic model in the sense that it is larger, wider, slightly taller and with more wing area.

The Saab 340B AEW&C is powered by two General Electric CT7-9B turboprops of 1870 hp with a Dowty Rotol (or Hamilton Standard) 14RF19 four-blade constant speed propeller each, allowing the airplane to reach a cruise speed of 522 km/h (325 mph). The Saab 2000 AEW&C also has a different powerplant, being 2 Allison/Rolls Royce AE 2100A turboprop engines of 4,591 hp with a Dwoty Rotol six-bladed constant speed propellers each, having improved performance than the 340B version: for instance, the cruise speed it can reach is up to 629,68 km/h (391,26 mph).

Given the role of the airframes, both are fitted with an Ericsson Erieye (PS-890) radar installed above the main airframe, with a range of S-band, 3 GHz (GigaHertz) with a range of 160 degrees on each side. The radar is a rectangular pod, in contrast with the radars one would see on more classical AEW&C planes (for example the Boeing E-3 Sentry or the Ilyushin A-50). The radar has a range of 300-400 km capable of detecting sea and airborne targets.

History

The A 340B AEW&C (S 100B Argus) came to be with the idea of having a Swedish modified AEW&C asset and an alternative to the comparatively more expensive Boeing E-3 AWACS. The Flygvapnet was already operating with a Saab 340B for VIP transport, designated TP 100A, and that same airframe was to be the basis for the new airborne defence and air control radar. By the mid-90s, the first unit entered in service with the Flygvapnet. A total of six airframes were ordered: four with the radar already installed and two without the radar, prepared to have it installed when needed and serving as VIP transports during peacetime. As mentioned above, the Saab 340B AEW&C (S 100B Argus) is based upon the commercial airliner Saab 340B, which is a good platform given its structural characteristics, avionics, and performance. This airframe began its development in the 70s, with the propulsion system that it has being chosen as it was more economic than the jet propulsion system back then. It is reported that cost/efficiency considerations and the effects of the 1973 Oil Crisis made the company to pick the turboprop propulsion system. The US Airline Deregulation Act of 1978 gave further impulse for the basic model to be developed. This airplane was developed and built jointly with Fairchild Aircraft, mainly due to the fact that Saab thought the production capacity would not be enough. As a result, from 1980 to 1987, Fairchild was tasked with manufacturing the wings, the tail, and the engine nacelles. Saab, in turn, was tasked with manufacturing the main airframe, covering the 75% of development costs and the system integration and certification. The first Saab 340 flew in 1983, with the first airplane serving with an airline in 1984. After Fairchild ceased operations, Saab began to fully manufacture the Saab 340, doing so until 1999. The Saab 2000 came to be due to a decision in 1988 by Saab to develop an elongated version of the Saab 340 capable of carrying up to 50 passengers, having the same economic efficiency along with better climbing performance. Its first flight was in 1992, entering into service in 1994.

Currently, the S 340B AEW&C (S 100B Argus) operates in the Flygvapnet with 4 units sporting radar equipment and two additional units serving as VIP transports, ready to have the radars installed when needed. Its production was also finished in 1999, with 12 AEW&C units built: six for the Flygvapnet, 2 for the Royal Thai Air Force and 2 for the Pakistan Air Force, with 2 more under production for the United Arab Emirates Air Force. 2 modified airframes were loaned for the Hellenic Air Force from 2000 to 2003, while Greece received two Embraer RJ-145 AEW&C aircrafts fitted with the same Ericsson Erieye radars. It is noteworthy to state that of the basic airliner version, 460 units were built. Of the Saab 2000 airliner version, 63 were built; in turn, the Saab 2000 AEW&C version was introduced in 2010 for the Pakistan Air Force, with 8 units built so far and operating with the Pakistan Air Force, the Royal Saudi Air Force and the United Arab Emirates Air Force. Three more units would be delivered for the Pakistani Air Force.

Design

The Saab 340B AEW&C design is based on the Saab 340B commercial airliner, while the Saab 2000 AEW&C is based on the Saab 2000 commercial airliner. As such, the airframe is the basically the same except that the former has the radar placed above the airframe, and other electronic equipment installed in the airplane. The airplane is of a dihedral wing design, which  means the wings are placed at the base of the airframe and angled upwards. It had two turboprop engines and an airframe built entirely of aluminium with the same construction techniques other Saab military fighters had: usage of bonding instead of rivets, reducing the overall weight of the airplane. It also has wider horizontal stabilizers, a vibration control system in the cabin to reduce the noise from the engines, and more powerful engines (the two General Electric CT7-9B turboprops of 1870 hp).

The wing and the horizontal control surfaces or stabilizers are dihedral, with the angle of the former being more prominent than the angle of the main wings. Both the wings and the horizontal stabilizers are both of trapezoid shape, being very thin – or simply not having that much of surface area. The engines are located at a quarter of the main wings, close to the main airframe. The main wings are located at the middle of the airframe, with the airframe being of tubular shape. The bow section of the airframe has a shape that varies according from the view or perspective. From an upper view, it has a parabolic nose cone; from a side view the shape is divided, with the area between the very roof and the windscreen having and inclination of around 38 degrees negative, and from the lower section of the windscreen to the tip of the nose, an angle of 30 degrees negative. The tip of the nose from a side view is placed at the lower section of the airframe, with the interior bow section from where the frontal landing gear is placed, to the tip, having an angle upwards of 10 degrees. The central section of the airplane is of cylindrical shape.

The aft or stern section of the airplane comprises the horizontal and vertical control surfaces, and two ventral tails fins. The tail is of conventional type with a sort of “double-delta” configuration; this is, the surface having at the forward area different angles. The forward section of the tail, from the central area of the airframe to the area where the horizontal control surfaces are placed, has an angle of nearly 15 degrees. From the aforementioned section to the tip of the tail the angle is of 45 degrees. From an upper view, the rear section is of conical shape, whereas from a side view the upper area of the aft section is lightly going downwards, and the interior part has an upwards angle of around 15 degrees. The ventral fins are placed right beneath the horizontal control surfaces. The rudder dominates half of the tail. And there is an elongating radome at the very rear part of the aircraft. The landing gear is of tricycle configuration, with the frontal landing gear placed at the nose cone (beneath the cockpit) and the two landing gear trains placed beneath the engine gondolas, them being retractable with storage inside the engine gondolas.

The Saab 2000 AEW&C has a similar structure to that of the 340, except that it is more elongated in width and length, the inferior section of the nose being entirely straight and the engines having more distance from the main fuselage. It also lacks the ventral tail fins the Saab 340B AEW&C (S 100B Argus) has.

The engines powering the aircraft are two General Electric CT7-9B turboprops of 1870 hp with a Dowty Rotol (or Hamilton Standard) 14RF19 four-blade constant speed propeller. Thanks to the powerplant, the airplane can reach a maximum cruising speed of 524 km/h (325,60 mph). The aircraft is fitted with devices to reduce the noise generated by the engines. The Saab 2000 AEW&C is powered by two 2 Allison/Rolls Royce AE 2100A turboprop engines of 4,591 hp with a Dwoty Rotol six-bladed constant speed propellers each, allowing a cruise speed of 629,68 km/h (391,26 mph).

The AEW&C version has the Ericsson Erieye radar placed above the central section of the airframe, supported by a series of pillars that connects it to the main airframe and with a slight inclination downwards from stern to bow. Ventral antennas are installed at the inferior area of the fuselage.

The canopy is of conventional type, typical of any commercial or transport aircraft, with two frontal windscreens, and a lateral windscreen at each side of the cockpit. The crew on the Saab 340 AEW&C (S 100B Argus) is normally six.

Fitting a civilian for defence duties

Perhaps surprisingly, the Flygvapnet lacked an airborne AEW&C system during the late Cold War, relying instead on either smaller airborne assets for surveillance or land radar stations. The Flygvapnet decided to close this gap by ordering Ericsson Microwave Systems to develop the PS-890 Erieye radar by the late 80s, with the airframe that would be used undergoing the first trials by the same period. This idea was, in fact, proposed back in the 70s but rejected. It was revived again in the Swedish Parliament (Riksdag) in 1982. As the Boeing E-3 Sentry AWACS was deemed too expensive, it is no surprise that the Saab 340 airliner was chosen by the Swedish Defence Materiel Administration as the platform for the airborne radar system. the Flygvapnet was already operating with a Saab 340B which was being operated as a VIP transport. In any case, it was a very good decision, considering the Saab 340B is a very economic airplane thanks to its powerplant’s configuration and the advanced basis avionics and electronics, which was hence an economic alternative to the E-3 Sentry. In combination with the Erieye radar, it makes a suitable platform for an airborne radar for Sweden. The Saab 2000 is an example of how this concept has evolved by incorporating the Erieye into an equally economical yet very capable airframe, which a derivative from the basic model.

The Eye of Odin

The radar installed in the Saab 340B AEW&C (S 100B Argus) is the Ericsson Microwave System Erieye PS-890 multi-mode active electronically scanned array (AESA) pulse-doppler radar, which makes the airplane a very remarkable AEW&C aircraft, considering its capacities. Its development began in 1985 after the Swedish Defence Materiel Administration, with a dummy dual-sided phased antenna being tested on the future platform, which was tested in trial two years later. It has 200 solid-state modules mounted in the antenna, with an S-band frequency and 3 GHz, with a ‘look’ on each side of 120 degrees and a reach of up to 300-400 km at an altitude of 6096 meters (20,000 ft). It has an altitude reach of up to 20 km (65,000 ft), yet leaves the nose and tail areas as blind spots. This shortcoming is compensated by the fact the radar – with this design in particular – can provide improved detection and better tracking thanks to the electronically scanned beam, at the point of being able to scan other areas while concentrating on a single target. Moreover, the PS-890 Erieye can detect and track fighters, helicopters, cruise missiles and even very small targets at the sea, as it has also a sea surveillance mode. Moreover, sectors deemed important can be scanned with different modes at a single moment, being capable of performing in electronically saturated environments and as an all-weather device, and can discern between friend and foes through its IFF capacities and devices.

This is suitable for the Flygvapnet considering that the dimensions it has to watch for are the air and the sea (even more as the Baltic sea is the most important body of water at the East, an area from which most of the threats have come historically, and even currently). As such, it can perform air and sea surveillance missions, Command and Control, Intelligence, control of own assets, surveillance and control of national borders, national assets and national economic zones, search and rescue, alert warning and air policing. The system is compatible with NATO airborne systems and standards.

The Erieye PS-890 radar has other electronic features, such as adaptive waveform generation with digital; pulse-coded electronic frames; signal processing and targeting, a track while scan device; low and medium pulse repetition frequency operating modes; frequency agility; target radar-cross section display; and air-to-air and sea surveillance modes.

Interestingly and despite the system being capable of receiving four multifunction workstations for airborne controllers, it can spare them as it has instead an onboard automatic systems datalink that can transmit to ground station the information gathered by the airborne radar, and with those same stations being capable of transmitting orders to the platform. The airplane and radar are both connected to the integrated Swedish Air Defence System and network StriC-90, thanks to this network, the airplane can maximize its operational performance, complementing in turn and even enhancing the capabilities of such system; this fact makes the Saab 340B AEW&C (S 100B Argus) airplanes very valuable assets in the Flygvapnet. And the same design of the radar module was the first of its kind, being also an alternative to the disc-shaped classical airborne radars. The radar developed by Ericsson is fitted in other similar airborne platforms such as the Embraer EMB-145/E-99 and the Bombardier Global 6000. It has now evolved into the Global Erieye airborne radar.

Variants of the Saab 340 AEW&C (S 100B Argus)

  • Saab 340 AEW&C / S 100B Argus – Airplanes having the PS-890/FSR-890 radar, and operated by the Royal Thai Air Force.
  • Saab 340B AEW&C 200 – Version fitted with the IS-340 Erieye radar
  • Saab 340B AEW&C 300 / S 100D Argus – Airplanes fitted with the upgraded PS-890/ASC-890 radar, capable of admitting from 1 to 4 operators.

Variants of the Saab 2000 AEW&C

  • Saab 2000 Erieye AEW&C – Version fitted with an airborne Erieye radar
  • Saab 200 MPA (Maritime Patrol Aircraft) – Version for Maritime Patrol and capable of performing ASW, ASuW, anti-piracy/anti-narcotics/anti-people smuggling, maritime counter-terrorism operations, search and rescue, support for special forces, SIGINT, and fisheries patrol, among other sea-based security tasks.

Operators

  • Sweden – The Flygvapnet operates four Saab 340 AEW&C (S 100B Argus) fitted with the Erieye radar, alongside 2 additional airframes serving as transport planes, ready to have the radar installed in case it is needed. The first airframes were received in 1994, entering fully in service between 1997 and 1999, and serving in the F16M wing at Malmstatt. Normally, there are no operators onboard, being rather used as a part of the integrated air defence network.
  • Greece – The Hellenic Air Force decided to acquire the Erieye radar system with 4 units to be installed in Embraer RJ-145 airplanes. While waiting for the newly acquired system to arrive, 2 Saab 340B AEW&C airplanes were loaned by the Greeks in the year 2000. The loaned units were modified, having two to three operator consoles, NATO IFF, communications and datalinks having a ground bases system for information processing fitted for Greek standards, but lacking the Swedish ECCM and also the cockpit display processing information from ground stations. These airplanes were returned to the Flygvapnet by 2003.
  • Thailand – The Royal Thai Air Force has two Saab 340 AEW&C that received in October 2012.
  • United Arab Emirates – The United Arab Emirates Air force requested 2 airplanes, with the units delivered being Saab 2000 AEW&C. Now operational.
  • Saudi Arabia – The Royal Saudi Air Force reportedly operates two Saab 2000 AEW&C for border surveillance.
  • Pakistan – This country operates four Saab 2000 AEW&C airplanes. 2 more are reportedly on order.

 

Saab 340 AEW&C – S 100 B Argus Specifications
Wingspan 70 ft 4 in / 21.44 m
Length 66 ft 8 in / 20.33 m
Height 22 ft 11 in / 6.97 m
Wing Area 450 ft² / 41.81 m²
Engine Two General Electric CT7-9B turboprops of 1870 hp with a Dowty Rotol (or Hamilton Standard) 14RF19 four-blade constant speed propeller.
Empty Weight 22,707 lb / 10,300 kg
Maximum Takeoff Weight 29,101 lb / 13,200 kg
Loaded Weight 7,500 lb / 3,401 kg
Climb Rate 2,000 ft / 10,2 m/s
Maximum Speed 285 mph / 528 kmh
Cruising Speed 285 mph / 528 kmh
Range 900.988 mi / 1,450 km
Maximum Service Ceiling 25,000 ft / 7,620 m
Crew 6
Electronics
  • An Ericsson Erieye (PS-890) radar.
  • Länk 16, HQII, IFF, secure voice, m.m.

 

Saab 2000 AEW&C Specifications
Wingspan 81 ft 3 in / 24.76 m
Length 89 ft 6 in / 27.28 m
Height 25 ft 4 in / 7.73 m
Wing Area 600 ft² / 55.7 m²
Engine Two Allison/Rolls Royce AE 2100A turboprops of 4152 hp with a Dowty Rotol six-blade constant speed propeller.
Empty Weight 30,424 lb / 10,800 kg
Maximum Takeoff Weight 50,625 lb / 22,800 kg
Loaded Weight 13,010 lb / 5,900 kg
Climb Rate 2,250 ft / 11,4 m/s
Maximum Speed 391,26 mph / 929,68 kmh
Cruising Speed 391,26 mph / 929,68 kmh
Range 2,301.55 mi / 3,704 km
Maximum Service Ceiling 30,000 ft / 9,144 m
Crew 7
Electronics
  • An Ericsson Erieye (PS-890) radar.
  • Länk 16, Self-protection systems, IFF/SSR, secure voice, ESM/ELINT, AIS; Command and Control devices such as consoles and a latest generation HMI.

Gallery

Saab 340 AEW Blueprint

 

 

Sources

Deagel.com. (2017). Saab 2000 AEW&C., Forecast International. (2000). Saab 2000 (Archived Report)., Fredriksson, U. (2004). Saab 340AEW. X-plane.org., Pike, J. (1999). S 100B Argus, Saab 340 AEW&C. FAS.org., SAAB. (n.d.). SAAB 2000 Erieye AEW&C Airborne Early Warning & Control., SAAB. (2009). SAAB 340B/Bplus. SAAB Aircraft Leasing. SAAB. (2013a). Erieye AEW&C Mission System., SAAB. (2013b). SAAB Airborne Surveillance Solutions. SAAB. (2015). High Quality and Support in Focus – Saab 340 & SAAB 2000., SAAB. (2016). The First Airborne Radar in Sweden Underwent Final Testing 20 Years Ago., SAAB. (n.d.). Erieye SAAB 2000 AEW&C System. The Spyflight Website. (2003). SAAB S100B AEW&C Argus. Images: 340AEW Royal Thai Airforce by Alec Wilson / CC BY-SA 2.0, 340AEW by Gnolam / CC BY-SA 3.0,  Side Profile Views by Ed Jackson – Artbyedo.com

Saab 18

Sweden, WW2, ,

sweden flag Sweden (1944)
Bomber – 245 Built

The Saab 18 is another example of Sweden’s efforts to produce an aircraft to safeguard its neutrality, considering that the same War and international political context prompted the Scandinavian nation to do so. Only that this plane was not devised to keep the skies of Sweden, but rather to protect the national territory from the air. Curiously, when WWII started, the Saab B 17 was given priority at the earlier stages of the war, as a dive bomber was considered more necessary than a light/medium bomber. This plane gave also important contributions to the development of the Swedish aeronautic and military industry, contributing in the development of ejection seats and of air-to-surface (or AGM) missiles; more specifically, anti-ship missiles. Despite being required to maintain Sweden’s neutrality and protect its territory, it entered in service in 1944, quite late to address the threat from Germany but ready to address the threat from the East and to serve at the early days of the Cold War, with distinction. It became also the standard bomber of the Flygvapnet.

The Saab B 18 is a light bomber and reconnaissance plane with three seats, two engines and a double tail, with a design similar to that of the Junkers Ju 86 and the Dornier Do 17 with the rounded shape of the vertical stabilizers. Or simply the very characteristic shape of double tail and double engine bombers of the era: this is, the cockpit placed at the frontal section of the plane and with the bow being made entirely of glass (normally the place of the bomber), and the cockpit being of a glazed offset type with the pilot and navigator. The wing has a trapezoid shape, being a straight leading edge type with the rear part being instead angled.

The Saab B 18 was initially intended to be powered by British-made Bristol Taurus engines. But it received in the end two types of engines during its career as the Taurus engines weren’t available, powered instead with two Pratt & Whitney R-1830 Twin Wasp radial engines of 1065 hp (the Saab J 21 had priority in receiving the Daimler Benz engines). Posterior versions received new powerplants as the Pratt & Whitney were deemed insufficient, hence receiving 2 Daimler Benz DB 605 of 1475 hp, enabling the plane to reach speeds of up to 570 km/h (357 mph), and making of the B 18 one of the fastest light bombers producing during the war. The powerplant was not the only modification the B 18 suffered during its service with the Flygvapnet, as the initial configuration of armament of 3 x 13,2 mm machine guns was changed to a set of one 7,92mm gun and 2 X 13,2mm machine guns (B 18B). Another re-configuration was the instalment of 2 X 20mm cannons and a 57mm gun (T 18B), along with rockets instead of bombs. Noteworthy to point out that the B 18 could carry up to 1,000 kg of bombs in the compartment and 8 x 50 kg bombs at the wings. As reconnaissance and torpedo-bomber variants were developed (though the last one was never put into service), the versatility and adaptability of the B 18 was made evident, at the point of being the platform for testing the Rb 302 anti-ship missiles. The crew was also modified, as following versions needed only two crewmen as rockets were introduced, suppressing the bomber.

Both versions (B 18B and T 18B) received another modification of armament in the 50’s, as they were fitted with rocket launchers allowing a maximum of 4 rockets on each wing, and even another rocket launcher allowing 2 or 4 rockets under the nose. The bomb sight was also equipped with an automatic reflex sight for rocket firing. This conversion meant that the B18B and the T18B would have increased – and more specialized – attack roles. Also, both the B 18B and the T 18B received ejection seats, maximizing the safety of the crew operating with these air assets. In addition, some B18 B units were fitted with two radars (a radar altimeter PH-10 and a search radar PS-18/A, which was a US Navy AN/APS-4 naval radar) for target designation and identification.

This airplane was purposed at replacing the Junkers Ju 86 in service with the Swedish Air Force back then, basing the requirement for a fast bomber with a crew of three. This was later on changed to a bomber having a crew of 3, a bomb payload of up to 750 kg (1653,46 lb), capable of reaching speeds of 500 km/h (310,68 mph) and to be used as a long-range reconnaissance, torpedo-bomber and heavy fighter. The fact that the B 18 ended in serving with the Flygvapnet was a sheer product of luck, as the competition’s design (the GV8 proposed by the competing AB Götaverken) was capable of meeting the requirements. Yet its costs and the departure of Götaverken’s chief designer resulted in Saab awarding the contract in 1938. As development began, many Americans reportedly took part in the design and development process, resulting in the B 18 having some “American traits” in the design. As a result, the B 18 development had a Swedish and an American chief designer: Frid Wänström and Carl Haddon, respectively.

The development process was delayed by two factors explaining the reasons of the Saab B 18 entering in service relatively late: first, the abovementioned shifting in priorities once the war started, with the Saab B 17 dive bomber receiving priority over the Saab B 18. And second, a change in requirements from a light bomber to a medium bomber, which ended in increasing the development time. The first flight took place in 1942, entering in service in 1944 with two initial versions: the B 18A bomber and the S 18A reconnaissance versions. A torpedo-bomber and later attack plane (T 18B), and a dive bomber (B 18B) were developed, receiving ejection seats.

After WWII and in the wake of the Cold War, the B 18B had a very interesting career, as the increase of the Soviet threat asked for reconnaissance missions; in 1945 and 1946 the B18 B was used to reach the Baltic coast and take pictures of every Soviet vessel, meeting Soviet fighters almost every time.

244 units were produced with the Flygvapnet being the sole operator until 1959, year in which the Saab 32 Lansen replaced the B 18: 62 units of the B 18A, 120 units of the B 18B, and 62 units off the T 18B were built. A single surviving airframe is displayed at the Flygvapenmuseum.

Design

The design of the B 18 is very typical of the pre-WWII double-tail light or medium bombers, having some interesting features despite its conventional sight at first glance. The B 18 is a straight leading edge wing airplane, with the engines placed at the first half of the wings. The fuselage was entirely made of metal, with fabric covering the control surfaces, and having the armor being integrally part of the structure.

The most remarkable areas are the canopy, the bow section, and the rear horizontal stabilizers, connecting the two vertical stabilizers with the main airframe. Regarding the canopy and bow section, the canopy is not placed at the longitudinal middle of the plane as it is normally placed, being instead an offset type at the left side. There, the pilot and the navigator were stationed, with the navigator seat being placed backwards. In addition, the bow section had a glazed tip where the bomber was stationed. Reportedly, such scheme improved the visibility for the pilot. The nose of the T 18B version was slightly modified. And the bow inferior section is not entirely straight, having instead an undernose gondola right before the wing-roots. The landing gear was of classic configuration, with the frontal landing gears retracting into the engine gondolas, while the small rear landing gear was placed at the stern of the bomber, right before the horizontal and vertical stabilizers area. In turn, the horizontal stabilizers are of a ‘butterfly shape’, having at the tips the two horizontal stabilizers; the rudders occupied the whole posterior area of the tails. The shape of the vertical stabilizers is of an isosceles trapezoid.

The wing is a mid-wing (cantilever) leading edge wing, with a shape of a right trapezoid and where the two engines are installed, along with the main fuel tanks. In some versions, there was a gun or a cannon installed at one of the wing-roots. The engines, depending of the version, were either a couple of Pratt & Whitney R-1830 Twin Wasp radial engines or a couple of licensed-built Daimler Benz DB 605 liquid cooled inline V-inverted engines. Depending of the installed engines, the air intake might be located below the engine gondola or above the engine gondola. Normally the earlier versions of the B 18 can be identifying by the intakes placed above the engine gondola. The Daimler Benz engine gave the B 18 a quite remarkable speed for a plane of its type back then, being among the fast ones with speeds of 575 km/h (357 mph). Such speed would provide an advantage for attack and reconnaissance missions. Reportedly, the T 18B version could reach speeds of up to 600 km/h (372,82 mph). The propellers of the B 18 where a three-bladed type.

The armament configuration also varied from version to version. The initial configuration was of 3 x 13,2mm machine guns, one firing forwards at the wing root, another firing also forwards at the nose, and another at the rear. This set was then changed for a set of one wing root 7,62mm machine gun and two 13,2mm guns, and then it was changed for a set of a front-firing 57mm Bofors gun at the undernose gondola and 2 x 20mm guns. The B 18 could carry up to 1,000 kg (2,200 lb) bomb and the bombs compartment and up to 8 x 50 kg (110 lb) bombs at the wings. This type of offensive armament was also changed, as it was first modified to carry a torpedo, which never came to be operational, and then it carried up to eight air-to-surface rockets. The B 18 was also used to test the Rb 302 anti-ship missile. The reconnaissance version was fitted with various cameras to perform its mission, along with a radar.

The B 18 was among the first planes in receiving ejection seats, as its high attrition rate made the Flygvapnet to implement such measure for the sake of the crew’s safety. The fact that it had ejection seats and capacity to carry missiles, along with its speed and un-conventional design, makes the B 18 a very interesting design made by a neutral nation during WWII and the early Cold War.

A Versatile Guardian of the Swedish Land

The B 18, although entering quite late to have a remarkable role in defending Sweden’s neutrality as WWII unfolded, it became a very valuable asset for the Nordic nation at the last stage of the war, when the Soviet Union became stronger and advanced towards the West, with the Cold War highlighting the threat it posed to Sweden. Not only its speed and considerable armament made the B 18 an air asset to be reckoned with, but also its versatility and adaptability, let alone its flexibility. The design allowed the installation of new engines that increased the speed of the B 18, as well as a change of armament while in service, at the point of serving as a test bed for one of the earlier anti-ship missiles, the Rb 302. These modifications allowed the B 18 to become very effective bomber and ground-attack planes, and even to serve as a reconnaissance plane capable of approaching or even penetrating Soviet airspace for its missions, facing quite often the Soviet fighters.

Striking at Speed

One of the characteristics that made the B 18 an airplane to be reckoned with was beyond any doubt its speed, especially after the Daimler Benz 305. The B 18B could reach speed of 570 km/h (357 mph), and the T 18B, the most powerful version in terms of firepower, could reach speeds of up to 600 km/h (372,82 mph). This was an advantage when it came to perform bombing or strike attacks with rockets, as the B 18 could have hit any advancing enemy ground forces formation with hit-and-run tactics or simply by direct strikes with devastating effects. Curiously, the S 18A was the slowest version, with speeds of up to 465 km/h being the maximum speed; this can be explained by the fact it was powered by the previous Pratt & Whitney engines, as the S 18A was a direct modification from the B 18A, which was (under)powered by such engines. Nevertheless, as the powerplants were enhanced, the B 18 became a very fast medium bomber. And it could have posed a serious threat to naval surface units approaching the Swedish coast.

Variants of the Saab B 18

  • 18A – Two prototypes powered by Pratt & Whitney R-1830 Twin Wasp engines of 1065 hp.
  • B 18A – This version became the first series version of the B 18, powered with the abovementioned Pratt & Whitney engines. Armed with 3 x 13,2 mm machine guns and up to 1400 kg (3086.47 lbs). 55 units were reportedly converted into the S 18A reconnaissance version in 146-47. 62 units delivered.
  • S 18A – A modified version of the B 18A for reconnaissance purposes, replacing the Caproni Ca 313 (S16) reconnaissance plane in service back then. It was fitted with a varied array of cameras: 3 high-altitude 10/92 and 5/25 cm cameras, 1 panoramic 10/105 cm camera and a 13/30 cm night camera. This version was also fitted with a PS-18A (An American-made AN/APS-4) maritime surveillance radar, with 36 units having this radar installed in pods under the nose, and serving as maritime reconnaissance airplanes.
  • Saab 18B – A single prototype powered with the Daimler Benz DB 605B.
  • B 18B – A dive bomber version powered by the new Daimler Benz DB 605B of 1475 hp engines. It was later on modified to carry up to 8 air-to-surface rockets, becoming an attack plane. Armed with a 13 mm machine gun and a 20 mm gun plus the 1400 kg (3086.47 lbs) payload of bombs, and later on the 8 air-to-surface rockets. A dive bomb sight m/42 developed by Saab engineer Erik Wilkenson maximized its attack capabilities. Reportedly, some B 18B received a PS-18A radar. This version received ejection seats, and had the crew modified, reducing it to two (pilot and navigator/radio operator). 120 units delivered.
  • T 18B – A projected torpedo-bomber to serve as an anti-ship asset, it ended in being a ground-attack plane thus receiving an armament of a 13mm machine gun, 2 x 20mm guns and a 57mm Bofors cannon at the undernose gondola, receiving later on air-to-surface rockets. This version also received ejection seats. 62 units delivered.

Operators

  • Sweden
    The Flygvapnet was the sole operator of the B 18, which entered in service in 1944 with 62 units of the B 18A model, followed shortly by 120 units of the B 18B that were initially purposed as dive bombers, developed later on into the T 18B with 62 units, which served as a ground-attack plane. The T 18B, in turn, was initially purposed to be a torpedo-bomber, but given problems with the new payload, received instead rockets hence serving as attacker. Some airframes were modified to be the S 18A reconnaissance plane, performing reconnaissance missions off the Soviet Baltic coast in the aftermath of WWII. It remained in service until 1958, year in which the Saab 32 Lansen replaced the B 18. It was used for testing the Rb 302 anti-ship missiles. The B 18B operated in 4 squadrons from 1944 to 1958: F1 Västerås, F7 Såtenäs, F14 Halmstad, and F17 Kallinge. The T 18B torpedo-bomber/attack aircraft operated also in the F17 Kallinge from 1948 to 1958. The S 18A operated in three squadrons in the same perios of time: F3 Malmen, F11 Nyköping and F 21 Luleå. A single B 18B recovered from a lake remains as a museum exhibition.

Specifications (B-18B)
Length 13.23m / 43ft 5in
Wingspan 17m / 56ft 9in
Height 4.35m / 14ft / 3in
Wing Area 43.75m2 / 470.92 ft2
Engine 2 X Daimler Benz DB 605 of 1475hp (some were licensed-built versions made by Svenska flygmotor AB).
Maximum Take-Off Weight 8800kg / 19,401 lb
Empty Weight 6100 kg (13,448 lb)
Loaded Weight 8140 kg (17,948 lb) (B 18A)
Maximum Speed 570Km/h / 357 mph
Range 2600 km /1,616 miles
Maximum Service Ceiling 9800m / 32,150ft
Crew 3 (2 in the T-18B)
Armament
  • A 13mm machine gun; 20mm cannon
  • A 13mm machine gun; 2x 20mm cannon; a 57mm gun (T 18B)
  • Up to 1400kg of bombs and rockets (the T18 B was intended to carry a torpedo or a mine, but it ended in having a payload of rockets)

Gallery

SAAB B18B

Sources

Arboga Robotmuseum. (2017). Rb 302. Arboga Robotmuseum., Aviastar.org (n.d.). Saab 18. 1942. Aviastar.org., Hertze, S. (2017). B18, B18A, B18B, T18B, S18A, Saab 18. Arboga Elektronikhistorika Förening AEF., Frederiksson, U. (2005). Saab B 18, the Swedish Air Force’s last propeller combat aircraft. X-plane.org., Henriksson, L. (2010). B18–Saab 18 (1944-1959). Avrosys.nu., Pilotfriend. (n.d.). Saab 18., The Spyflight Website. (2003). Swedish Cold War Reconnaissance., wwiivehicles.com. (2017). Sweden’s Saab B18, Saab 18 bomber. wwiivehicles.com., Saab 18. (2017, May 17). In Wikipedia, The Free Encyclopedia., Images: Saab 18 Forward View by Johnny Comstedt / CC BY-NC-ND 2.0, Side Profile Views by Ed Jackson – Artbyedo.com

 

Saab sk60A - F 5 Ljungbyhed - 60113 Side Profile View

Saab 105

Cold War, Sweden, , , , ,

sweden flag Sweden (1967)
Trainer – 192 Built

The Saab 105 is a high-wing, twin side-by-side seat configuration, two engine-powered training and multi-mission jet, with swept-wings. This airplane (later denominated as Sk 60 by the Swedish Flygvapnet) was the product of a private venture by the company, which and after witnessing the success of the S 35 Draken, decided to implement a program with its own funds to develop a new training plane, with military purposes and eventually, civil purposes. The Saab 105 is, in fact, a multi-mission aircraft, in lieu with the operational framework Saab and Sweden normally contemplates for its aircraft. For instance, it can perform missions of training, liaison, ground attack, reconnaissance and limited interception. In regards to civilian use, the small jet was intended to be a four or five-seat business jet, but this plan met no success, making the Saab 105 a military machine and the company to aim at the military market (until the arrival of the Saab 340 and the Saab 2000, the company would not venture into the civil market, although Saab ventured into this market in the Saab 90 Scandia in the 40’s and 50’s). It replaced the de Havilland Vampires that served in the Flygvapnet as training jets.

Saab sk60A - 60140

Noteworthy to point out that this aircraft was a milestone for European aerospace industry, for it was the only small European design in being powered by turbofan engines, increasing the prospects of customers – yet the foreign sales were rather modest, with Austria being the only country in exporting the jet. Nevertheless, it managed to have the attention of the Flygvapnet, placing an order for at least 100 units of the jet, and even sponsoring further development of the jet on an initial training version.

Development

The development programme started in 1961, with the prototype having its first flight in 1963, where the airplane revealed to have very good handling qualities and good manoeuvrability, capable of performing acrobatic manoeuvres. The original powerplant, the Turbomeca Aubisque was tested at the engine’s factory in France with one prototype delivered there solely for that purpose, being later on produced by Volvo under license as the RM9. The powerplant would be updated as time went by, with the Swedish-operated Sk 60 receiving a Williams International FJ44 engine (manufactured by Volvo as the RM15 and fitted with Auxiliary Power Reserves), mainly due to the Aubisque Engines reaching the end of their operational life, and tight defence budgets.

sk60a-trainer-display
In 1966, the Saab 105 entered in service with the Flygvapnet following the Swedish government authorization to incorporate 130 aircraft, with three main variants having specific missions each: the Sk 60A for training and liaison with a four-seat configuration; the Sk 60B for light attack mission with the cockpit having a twin side-by-side seat configuration; and the Sk 60C with ground attack and reconnaissance missions, equipped with cameras at the nose. There was an improved version to be exported to Austria (the Saab 105Ö/ÖE), with better powerplant – a General Electric J85 – and improved avionics, as well as reinforced wings and optimized for high-altitude operations.
The Saab 105 is a four-seat or twin side-by-side seat multi-mission aircraft, having two engines, high-wing, a tail on a T shape and the tail being very wide. The wings are swept-wings, with the cockpit placed very bow of the aircraft and right before the wings, with the engine air intakes placed beneath them and at the forward edge. The canopy is if of bubble type, although it has no free rear vision, as the canopy does not stand above the fuselage. The engine has been updated from time to time, as well as the avionics, with the Austrian version being the version receiving the most important updates. In addition, the Saab 105 is capable of carrying a varied array of armament, such as 135, 127 or 75 mm rockets, Saab Rb05 ASM missiles, bombs and cluster bombs, and 30 mm or 12,7mm (training) guns at gun pods for ground attack missions. Cannons and AIM-9 Sidewinder/ Rb24 missiles can be used for the limited air defence and interception role, and cameras and radiation detecting equipment for atmospheric sampling in reconnaissance missions.

Service

As the Saab 105 entered in service with the Flygvapnet and the Österreichische Luftstreitkräfte in 1966 and 1970, respectively, with 150 units in Sweden and 40 units in Austria, making a total of 190 units (including the prototypes), where they are still in service with both air forces. Thanks to its manoeuvrability, the Saab 105/Sk 60 was used in acrobatic teams at both nations: in Sweden, it is used by the display team Team 60 of the Flygvapnet, whereas in Austria it was used by two Österreichische Luftstreitkräfte teams, Karo As and the Silver Birds. A replacement for the Saab 105/Sk 60 is now being considered, as it has been in service for 40 years, while one of the prototypes is now a museum display since 1992. Nevertheless, an agreement between Saab and the Swedish Armed forces was reached in 2015 in order to support and keep the Sk 60 airworthy until 2020.

Design

The design of the Saab 105/Sk 60 is conventional, although it has some remarkable characteristics that makes this jet to be very different from other airplanes of similar type. The airplane is mate entirely of metal. For instance, the nose is relatively small from longitudinal perspective, yet being wide enough to accommodate the frontal wheel of the landing undercarriage. On the reconnaissance version, its size is increased in order to accommodate the camera equipment and other instruments. The canopy and cockpit are also unique – similar to the Bae 167 Strikemaster and the Hunting (Percival) P.84 Jet Provost in shape – with a ‘bubble’ configuration where two or four crew can accommodate, although it is normal to have a crew of two in training missions. The seat configuration was a twin or side-by-side seating, and in some versions, 4 seats were accommodated in the cockpit.

Noteworthy to remark, the canopy takes more than the half of the height at the bow. Right after the cockpit and canopy the radio antenna is installed above the fuselage, in the same area where the engine air intakes and the wing both start. The wing is a high swept-wing, although is not perfectly strait, as it has a depression angle from the base to the wingtip. Furthermore, the leading edge is swept, while the area of the ailerons and flaps is slightly swept. The wing accommodates six hardpoints (three on each wing) that allows the airplane to carry a varied array of weaponry and depending of the mission it was tasked with.
The engines – the Saab 105 was normally powered by two engines: a couple of Turbomeca Aubisque Turbofan, a couple of Williams FJ44, or a couple of General Electric J85 engines – were placed at the sides of the fuselage, and occupying the whole central section of the jet. The exhausts were placed right before the tail group began, hence the T shape of the tail, with the horizontal stabilizer and elevators placed on top of the vertical stabilizer. The vertical stabilizer in turn, is having a considerable area, giving the tail its characteristic ‘big’ shape, with the rudder having a similar ample area, equal to the Canadair CL-41G-5 Tebuan. Each side of the tail is having a trapezoid shape.

saab-sk60a-in-flight-2

The landing gear is of tricycle configuration, with the frontal wheel located at the nose, and the rear wheels placed at the central area of the fuselage, right beneath the wing and the engines, being retractable.

In regards to the armament, it was normally varied, depending of what were the mission to accomplish. The initial configuration of training and liaison would be unarmed (except for the 12,7mm training guns), yet for its secondary ground attack roles it would be armed with 30 mm or 12,7mm (training guns) guns installed at pods, fitted in the wings, unguided rockets – of 135, 127 or 75 mm –, bombs – either free fall or cluster bombs – and two Saab Rb05 air-to-ground missiles. As it is capable of limited air defence and interception, it can carry the 30mm or 7,62mm guns at the pods and AIM-9 sidewinder/RB 24 air-to-air missiles. Cameras and radiation detecting equipment for atmospheric air samples were the normal equipment for reconnaissance missions. Noteworthy to remark that additional fuel tanks were never intended for use, therefore the wings never carried such equipment. A publicly known Sk60 received important updates in avionics and navigation systems in 2013, constituting itself a new version (Sk 60AU).

A Private Venture

The Saab 105/Sk 60 as the idea of developing a small high-speed business jet featuring a delta wing and cannards with 5 seats, but also due to the success of the Draken and the need for developing a trainer that could train the Flygvapnet pilots for the J 35, moreover when the de Havilland Vampires were not suitable for the task. This realization, along with the fact that the proposed business jet found no fertile ground for success, made of the new Saab 105 to be more a military plane, although some of the 150 built jets were used as liaison and VIP transports. At the same time, the Flygvapnet was requiring new training aircraft, selecting the Saab 105 above other – good – options, such as the Fouga Magister or the Macchi MB.326, to name a few. As a result, the Saab entered in service with the Air Force sponsoring further its development. Some year after in entered in service, Saab engaged in a campaign to export the Sk 60 to other nations – mainly those that were neutral during the cold War, curiously – such as Finland, Switzerland and Austria. Only the last one bought 40 Sk 60, which were enhanced versions of the original model and fitted for Austrian service.

A Small but Versatile Jet

The Saab 105 might look a modest, uninteresting aircraft at first sight, but like all Saab models, it is a very capable jet with very good flying characteristic, being its manoeuvrability the most remarkable one. It was also deemed to be easy to fly, It is also a multi-mission airplane, capable of adapting to different missions. For instance, it can perform training and liaison missions in principle, but it is also capable of executing ground attack, reconnaissance and atmospheric air sampling, and even limited air defence and interception (especially the Austrian units). It has been in service with both the Swedish and Austrian air forces for about 46-50 years, being among the airframes serving for a long period of time with any air force. As a result of its manoeuvrability, it was used by acrobatic teams in both Sweden and Austria.

Variants of the Saab 105/Sk 60

  • Saab 105 – The prototypes of the trainer and liaison airplane. Two prototypes built
  • Sk 60A – The first production series, configured as two-seat trainer and liaison jet, with 149 units built.
  • Sk 60B – The second version configured for ground attack missions and made from modified Sk 60A airframes, incorporating armament.
  • Sk 60C – The third version, configured for ground attack and reconnaissance mission, fitted with a camera (a Fairchild KB-18 panoramic fil camera) that elongated the nose, since it was installed there. A prototype and 29 converted airframes from the Sk 60A comprised the quantity of this version.
  • Sk 60D – Saab reportedly configured the Saab 105 as a four-seat liaison transport, with the combat seats replaced by four airliner-type seat lacking use of parachute, or even four seats of the same type that would allow the use of parachutes by the crew. 10 Sk 60A airframes were modified to give way to this version in the mid-70’s, receiving the same ‘splinter camouflage’ painting applied to the Saab S 37 Viggen
  • Sk 60E – Similar to the Sk 60D version, only that it was fitted with airliner-type instruments, including an instrument landing system. It trained Flygvapen reserve pilots in flying commercial aircraft, used later on as Sk 60D transports.
  • Sk 60W – Intended programme in 1993 to upgrade the Sk 60, were a new powerplant (Williams Rolls FJ44 turbofan engines) and digital engine control were to be installed, as well as LCD altitude indicators. Implemented in 1995, the Sk 60 powered by these engines were denominated informally as Sk 60W. 115 Sk 60A, Sk 60B and Sk 60C were upgraded, while the Sk 60D and Sk 60E were grounded and used for part cannibalization.
  • Sk 60AU – A new version of the trainer, being a modification of an existing airplane, it incorporated new avionics and instruments. Among the upgrades incorporated, there is a GPS, new radio, new audio warning systems, new navigation systems and information on a similar manner as in the JAS 39. Introduced in 2013 with a single unit modified publicly known at F 17 Ronneby.
  • Saab 105XT – An improved Sk 60B powered with a General Electric J85 Turbojet engines made from the second Saab 105 prototype, purposed to be an export demonstrator. The engines, noteworthy to point out, yielded speed of up to 970 km/h, making it a subsonic aircraft.
  • Saab 105D – A proposed refined business jet version, but it was cancelled as there were no takes and the idea was out of time.
  • Saab 105G – A revised version of the Saab 105XT that featured new avionics, such as a precision navigation and attack system, enhanced J85 engines and modified wings, with only one units from a modified Saab 105XT
  • Saab 105H – Proposed training version for the Swiss Air Force. As this air force rejected the project, none were built.
  • Saab 105Ö (105ÖE) – An export version made for Austria and based on the Saab 105XT, entering in service with the Österreichische Luftstreitkräfte in 1970 and 1972, replacing the de Havilland Vampires and Saab J 29 Tunnan this air force was operating with back then. Powered by the General Electric J85 engines
  • Saab 105S – A proposed trainer demonstrator for the Finish Air Force, as it was requiring a trainer in the mid-70’s. Finland decided instead to purchase Bae Hawk trainers.

Operators

  • Sweden
    The Flygvapnet operated the Saab 105 under the denomination of Sk (Skola) 60(A). 150 units served with the Swedish Air Force in 1966 and for unarmed training missions. They began to operate at F 5 Ljungbyhed and the F 16 Uppsala flying schools. At the earlier 70’s the Sk 60A were modified with the installation of hardpoints at each wing, allowing them to operate also as light attackers. 46 units were modified and denominated Sk 60B. At the same time, 30 Sk 60A were modified into the Sk 60C, allowing cannons pods and rockets, as well as the installation of a panoramic reconnaissance camera, serving in the abovementioned wings as well as in the F 21 Luleå, where a light attack squadron was stationed. In 1988-1991 and 1993 the Sk 60s suffered upgrades, mainly at the wing – which were reinforced – and the pilots’ ejection seats, as well as receiving new powerplants. The Sk 60D/E were kept out of any modernization programmes, used instead for cannibalization (or to use the aircraft as sources for spare parts). A single unit so far has been modified with new instruments and GPS devices in 2013 at F 17 wing Ronneby, constituting the Sk 60AU. Similarly, the builder and the air force reached an agreement in 2015 to keep the trainer airworthy and with any maintenance support for this purpose, until 2020.
  • Austria
    Operated 40 Saab 105Ö/ÖE were purchased, with 28 currently remaining. The Österreichische Luftstreitkräfte operates this aircraft mainly for training purposes, but also for other mission such as ground attack, reconnaissance (including radioactivity measurement), VIP transport and limited air defence and interception missions. The Austrian Saab 105 were noticeably operated when US president George Bush visited Austria, performing air patrols under the policy of air guard when a personality or important summits are taking place. It is still deemed a good tool for fighter training by the Austrian Air Force.

Saab 105 Specifications
Wingspan  9,5 m / 31 ft 2 in
Length  10,5 m / 34 ft 5,83 in
Height  2,7 m / 8 ft 9 in
Wing Area  16,3 m² / 175,5 ft²
Engine  2 x Turbomeca Aubisque (Volvo Flygmotor RM9), or 2 x General Electric J85-17B Turbojet, or 2 x Williams FJ44 (Volvo Flygmotor RM15)
Maximum Take-Off Weight
Empty Weight  2510 kg / 5,533 lb
Loaded Weight  2835 kg / 6,240 lb
Maximum Load  800 kg / 1,763 lb
Climb Rate  75m/s (Saab 105Ö/ÖE)
Maximum Speed  770 km/h / 360 mph at 6095 m (19,996 ft)
Range  1400 Km / 790 miles
Maximum Service Ceiling  13500 m /44,291 ft
Crew  2 (instructor pilot and student pilot) or 4 in case of liason/VIP transport mission (Sk 60D/E)
Armament
  • 6 harpoints allowing up to 700kg (1,543 lb) of payload: 2 x Saab Rb05 ASM missiles
  • 2 x AIM-9 Sidewinder/Rb24 AAM missiles
  • Pods for 30 mm or 12,7 mm cannons
  • 12 X 135mm, 127mm or 75mm rockets
  • 250kg (550lb) bombs, cluster bombs and rocket launcher pads.
  • The reconnaissance version was equipped with a Fairchild KB-18 panoramic camera at the nose, as well as radioactive air measurement instruments.

 

Gallery

Saab sk60A - F 5 Ljungbyhed - 60113 Side Profile View
Saab sk60A – F 5 Ljungbyhed – 60113
Saab sk60A - F 5 Ljungbyhed - 60140 Side Profile View
Saab sk60A – F 5 Ljungbyhed – 60140
Saab sk60A - 60088
Saab sk60A – 60088

sk60a-trainer-display

saab-sk60a-in-flight-2

Saab sk60A - 60140

 



Sources

Airheadsfly.com. (2013). Upgraded SK60 Operational. Airheadsfly.com., Charleville, J. (1996)., Nya SK 60: Inte W men A, B, C., FlygvapenNytt (4), 25., Das, W., & Otten, K. (n.d.). Saab 105 in Austrian Air Force. Dutch Aviation Support., Flygrevin. (2012). SAAB Sk-60 – flygande skolbänk. Flygrevyn (2), 2-6., Fredriksson, U. (2001). Saab 105 in Swedish service. X-plane.org., Försvarsmakten. (2013). F17 har fått en ny versionen av SK 60. Försvarsmakten., Globalsecurity.org. (2012). Sk60 / Saab 105 trainer/light attack aircraft. Globalsecurity.org., Goebel, G. (2016). SAAB Trainers: Safir, SAAB 105, & Supporter. Airvectors.net., Hultgren, O., & Moberj, T. (1998). Abstract, in Saab 105 “SK60” Re-Engine Programme. Defence Materiel Administration Testing Directorate. Linköping, Sweden. , Peterson, G. (1997). Saab 60 år. Saab 1937-1997: Dramatik och dynamik, FlygvapenNytt, (3) 6-17., Saab. (n.d.). 1960’s. Saab., Saab. (2015). SAAB Signs Sk60 Support Agreement with FMW. Saab., Sharpe, M (2001). Jets de Ataque y Defensa [Attack and Interceptor Jets, Macarena Rojo, trans.]. Madrid, Spain: Editorial LIBSA (Original work published in 2001)., Saab 105. (2016, October 8). In Wikipedia, The Free Encyclopedia. Images: Saab sk60A in Flight by Jim Calow / CC BY-ND 2.0, Saab sk60A in Flight 2 by John5199 / CC BY 2.0, Sk60A Trainer Display by Alan Wilson / CC BY-SA 2.0, Side Profile Views by Ed Jackson – Artbyedo.com

FFVS J 22

Sweden, WW2, , ,

sweden flag Sweden (1943)
Fighter Plane – 198 Built

FFVS J 22B at the Flygvapnet Museum
FFVS J 22B at the Flygvapnet Museum

The FFVS (Kungliga Flygförvaltningens Flygverkstad i Stockholm/Royal Air Administration Aircraft Factory in Stockholm) J 22 was a small light fighter airplane, and an exception to the mostly Saab-built airplanes, which were the ones equipping the Flygvapnet the most. But like those made by Saab during WWII and the early Cold War, this aircraft is a product of the defence needs that the war was imposing upon the Scandinavian nation. Although not so renown as its colleagues, this fighter proved to be a feat of Swedish capacities during dire times and tight resources, compensating its comparatively small size with good firepower and good performance. Of course, and like all of Swedish-made (and imported) air assets, it was purposed with giving Sweden with tools enough to defend its territorial and airspace integrity and security, let alone its neutrality. This under a locally built armament programme while facing restrictions to foreign advanced aviation technology.

A single-seat, single-engine airplane. Its design is conventional, yet the wings are placed further bow of the airframe, with a trapezoid shape. The nose is very similar to those of the American-made fighters, with a wide and cylindrical shape due to the shape of the engine. The cockpit was also placed at the bow section of the fighter, yet slightly aft the leading edge of the wing. The canopy was a bird-canopy design. The canopy hinged to the right side.

The J 22 was powered by a SFA STWC-3G 14-cylinder air-cooled radial engine of 1065 hp, which was an unlicensed version of the Pratt & Whitney R-1830 engine. A three propeller-blade composed the other propulsion element of the aircraft. The engine-propeller combination allowed the J 22 to yield speeds up to 575 km/h (360 mph), being this speed aimed to make the fighter comparable to the Messerschmitt Me109 and Supermarine Spitfire. The first version of the fighter (J 22A/J 22-1) was armed with a set of 2 X 7,9mm and 2 X 13,2mm light and heavy machine guns. The second version (J 22B/J 22-2) was armed with a set of 4 X 13,2mm heavy machine guns. As it not carried bombs or rockets as secondary weapons like most fighter designs of those days, it was a 100%-designed fighter.

The J 22 was developed aiming at providing Sweden with an air asset enough for it to defend its airspace, by providing the Flygvapen with a rather modern fighter. But it was also aiming at producing a new aircraft through a company established solely for this purpose, as Saab was already busy producing the Saab 17 and Saab 18 bombers. in addition, it was purposed with replacing many of the outdated fighter assets the nation had by the beginning of the war. Development began in 1940, with Bo Lundberg as both head of design and head of the newly established company (FFVS). Lundberg was already having experience as head of Swedish Air Commission USA, and as chief designer of Götaverken’s aircraft division that designed the GP 8 bomber and the cancelled GP 9 fighter. He was commissioned with designing a new fighter required to use the STWC-3G (Pratt & Whitney R-1830) engine, being small and light in size and weight, and interestingly, to be made of parts manufactured by a large number of subcontractors. The J 22 development, manufacturing and testing took place at the workshop of Flygtekniska Försöksansalten (FFA) near the Bromma airport. Both prototypes crashed during testing, due to pilot’s oxygen device and engine failures. The J 22 first flight took place in 1942

The J 22 entered in with the Flygvapnet in 1943, remaining in that until 1952, year of its retirement, with 198 fighters built from 1942 to 1946. During its service, it was well received by the pilots, thanks to its good manoeuvrability and responsive controls, capable of giving a fight to the Mustangs P-51 at heights up to 5000 meters (16,000 fts). It did not have stall problems at turns or straight forward course, and the second version (J 22B/J 22-2) was considered the best in terms of firepower. Moreover, the simple systems facilitated maintenance and service. The J 22 was reportedly comparable to the early versions of the Supermarine Spitfire and of the Mitsubishi A6M Zero. Three J 22 are preserved as static displays in museums.

Design

FFVS J 22A at an airshow circa 1990
FFVS J 22A at an airshow circa 1990

The design of the J 22 is a conventional one, being a small and lightweight airplane, whose shape is very similar to most US airplanes of the era. The fighter is a cantilever mid-wing design, with its structure being a mixed steel tube and wood construction (plywood) one. In fact, the tubular-steel framework and fuselage were having coverings of moulded plywood panels. The only drawback of the design was that forward visibility was poor.

The J22 wing has the average shape of most WWII-era fighters, a trapezoid shape. It was located slightly towards the bow of the airplane, containing the fighter’s guns and the fuel tanks. In addition, the air intakes were placed at the roots of the wings. The aft section of the airplane contained the vertical and horizontal stabilizers, with the rudder dominating most of the tail, while and as a result, the horizontal stabilizers were placed before the rudder. The landing gear, in turn, was also of classic configuration – two ‘legs’ with the wheel and a tailwheel – being also retractable and rotating, very similar to the Vought-Chance Corsair F4U. The only problem with the tailwheel was that, if left unlocked and able to swivel, it could result in ground-loops. Interestingly, the landing gear was designed to accept skies, that were never installed as snow-clearance service of the runways was improved.

The engine was a SFA STWC-3G 14-cylinder air-cooled radial engine of 1065 hp, an unlicensed copy of the American-made Pratt & Whitney R-1830 engine, allowing speeds of up to 575 km/h (360 mph). given the shape of the engine, the nose has the characteristic cylindrical shape of the American homologues. The propelling system was comprised of a three-blade license-built Hamilton standard propeller connected to the engine. Alongside speed, the J 22 was deemed a manoeuvrable and easy to control fighter with good performance especially at low altitudes. Furthermore, it had no stalling problems but the tendency to flip over its back if pulling hard when turning. It was considered capable to outperform the P-51 Mustangs, and be equal to the early versions of the Zero and the Spitfire. The armament had different configurations on the two main versions: The J 22A (J 22-1) was armed with 2 X 7,9mm and 2 X 13,2mm machine guns. The J 22B (J 22-2) was armed with 4 X 13,2mm machine guns. In both cases, the armament was placed at the wings. No secondary weapons were carried.

The canopy was of a bird-cage type, which hinged to the right to allow the pilot to enter and exit the airplane, with the windshield made of 6mm laminated Gremax or acrylic, and the center part being thickened with 60mm for ballistic protection. The gunsight was a fixed reflex sight.

Noteworthy to point out, that 500 hundred contractors produced 12000 of the 17000 total parts of the J 22.

A war-time solution for a non-belligerent nation

ffvs-museum-1The J 22 is also a product of the need to defend the airspace and the neutrality of Sweden, as modern air assets were required to meet this objective. By the beginning of WWII, Sweden was having 60 Seversky P-35 (of the 120 ordered), 60 Italian-made Reggiane 2000 and 72 Fiat CR. 42 biplanes – bought as a temporary measure – and old Gloster Gladiator fighters. As Sweden did never receive the remaining 60 P-35 and 144 Vultee P-66 Vanguard it ordered from the US, due to the embargo imposed to any arms delivered to any country but the United Kingdom after the invasion of Norway by Germany, in 1940.

As a result, Sweden bought the abovementioned Italian fighters to provide the Flygvapnet with some air assets, but it was deemed necessary to introduce up-to-date fighters. Initially, Sweden considered to buy additional fighters from abroad, such as the Finnish VL Mysky, the Soviet Polikarkov I-16 and even the Japanese Mitsubishi A6M Zero. But these options were having problems, such as not bing enough or being impossible to transport into Sweden despite being available, s it was the case of the Zero.

As a result, the FFVS was established, as Saab was already concentrating on the fabrication and development of bombers and fighters, with the sole purpose of developing and manufacturing a new lightweight fighter that would provide the Flygvapnet the needed modern air assets to keeps its neutrality in a world at war. Consequently, it replaced the Gladiator, the Severski, and Reggiane and Fiat fighters while other air asserts were received – like the Mustang P-51 – and the Saab J 21 was ready to enter into service.

The fast and small Viking warrior of the skies

Although the J 22 was a very small and lightweight fighter, it was a very capable one, proving itself to be able to undertake its purposed task: defend the Swedish airspace and neutrality. The secret of its good performance was its engine and structure. It was among the fast fighters the Flygvapnet had back then, reaching speeds of 575 Km/h (360 mph). It was also a manoeuvrable fighter, with a fast turning rate – it was even capable of getting the Mustang in the gunsight by out-turning It – with responsive controls. The altitude where it tended to perform the best was at low altitudes, with the performance decreasing at higher altitudes. Stall problems where rather absent, and it was an airplane easy to maintain and service by land maintenance crews.

Variants of the FFVS J 22

  • FFVS J 22A - 22185
    FFVS J 22A – 22185
  • J 22A (J 22-1) – First production series armed with 2 X ,9 mm M/39A (Browning M2) machine guns and 2 X 13,2 mm heavy machine guns. Operated until 1952. 143 delivered.

  • FFVS J 22B - 22280 Side Profile View
    FFVS J 22B – 22280
  • J 22B (J 22-2) – Second production series armed with 4 X 13,2 mm M/39A (Browning M2) heavy machine guns. 55 delivered.
  • S 22 (J 22-3) – Reconnaissance version (the S stands for spaning, or ‘reconnaissance’ in Swedish), equipped with a vertically mounted camera. Developed from J 22A (J 22-1) airframes in 1946, refitted as fighters in 1947. Operated until 1952. 9 airframes modified and refitted.

Operators

  • Sweden – The Flygvapnet operated the J 22 during the last half of WWII, being also in service during the earlier days of the Cold War, as it was retired until 1952. A total of 198 airframes were in service, being 143 of the J 22A version, 55 of the J 22B version and 9 airframes of the first version modified to produce the S 22 version, which served for a very short period of time as reconnaissance airplane. In 1945 all the J 22 were re-designated as J 22-1 for the first version, J 22-2 for the second version, and J 22-3 for the third version. These last airplanes were re-conditioned a year later as fighters. Three J 22 remain today as museum exhibitions in Sweden. It served with seven squadrons throughout its career: F3 Malmen; F8 Bakarby; F9 Säve; F10 Barkråka; F13 Bråvalla; F16 Uppsala; and F18 Tullinge. The S22 (J 22-3) served only in the F3 Malmen squadron.

 

 

J 22 Specifications
Wingspan  10 m / 32 ft 10 in
Length  7,80 m / 25 ft 7 in
Height  3,60 m / 11 ft 10 in
Wing Area  16 m² / 172,16 ft²
Engine  1 SFA STWC-3G (Pratt & Whitney R-1830) 14-cylinder air-cooled radial engine of 1065 hp
Maximum Take-Off Weight  2835 Kg / 6,250 lb
Empty Weight  2020 kg / 4,445 lb
Loaded Weight  2835 kg / 6,240 lb
Maximum Speed  575 km/h / 360 mph
Range  1270 Km / 790 miles
Maximum Service Ceiling  9300 m /30,500 ft
Crew 1 (pilot)
Armament
  • 2 X 7,9 mm M/39A (Browning M2) machine guns and 2 X 13,2 mm heavy machine guns located at the wings (J 22-1).
  • 4 X 13,2 mm M/39A (Browning M2) heavy machine guns located at the wings (J 22-2).

 

Gallery

FFVS J 22A - 22185
FFVS J 22A – 22185
FFVS J 22B - 22280 Side Profile View
FFVS J 22B – 22280

 

FFVS J 22B at the Flygvapnet Museum
FFVS J 22B at the Flygvapnet Museum
FFVS J 22A at an airshow circa 1990
FFVS J 22A at an airshow circa 1990

ffvs-museum-1



 

Sources

Aviastar.org. (n.d.). FFVS J22. 1942. Aviastar.org., Frederiksson, U. (2002). Saab J 21/A 21/A 21R. x-plane.org, Fridsell, M., & Waligorski, M. (2002). FFVS J 22 in Detail. IPMS Stockholm, Goebel, G. (2014). The SAAB J 21 & J 21R. Air Vectors., Henriksson, L. (2010). J 22 – FFVS J 22 (1943-1952). Avrosys., Hertze, S (2015). J22, J22A, J22B, S22-3, FFVS 22 Jaktflygplan, Spaningsflygplan. Arboga Elektronikhistoriska Förening., J 22 Memorial Flight. (2016). J 22 History. J 22 Memorial Flight., Lindqvist, R. (2013). J 22, FFVS J 22. Flygvapenmuseum., Palten, K. (2016). FFVS J 22. Flugzeuginfo.net., FFVS 22. (2016, June 26). In Wikipedia, The Free Encyclopedia.,Stenberg, D. (1976).Flygvapen 1926-76, FlygvapenNytt, (3) 8-20, Söderblom, B., Rassmusen, R., Söderberg, G. (n.d.). Flygplanrevy, (12 – 17)., Images: FFVS Museum 1, FFVS Museum 2 by Alan Wilson / CC BY-SA 2.0, FFVS Taxiway by Towpilot / CC BY-SA 3.0, Side Profile Views by Ed Jackson – Artbyedo.com

 

Saab J 21R - 21463 w/ Gun Pod Side Profile View

Saab 21 / 21R

Sweden, WW2, ,

sweden flag Sweden (1945)
Fighter / Attack Plane – 298 Built

The Saab J 21 is a peculiar airplane, not only because of its advanced features. This fighter in particular is one of the only two airplanes that were initially powered with a piston-propelled engine, then later modified to incorporate a jet engine using the same airframe and implementing very few modifications. This airplane is also the product of Swedish defence concerns and resourcefulness, as Sweden wanted to keep its neutrality and territorial integrity during WWII, electing to develop a domestic fighter program as access to foreign advanced technology was restricted.

Saab J 21A-3 in a Hangar
Saab J 21A-3

A single-seat, single-engine airplane that later became one of the first-generation jet fighters. Its design is a twin-boom tail pusher configuration. It had two longitudinal booms, attached to the main wing but extending backwards from the middle section of each wing, with the main body placed in the middle. Similar to the Lockheed P-38. This design also implements a rear mounted piston engine, otherwise known as a pusher configuration, which made engine modifications easy.

The piston-propelled version, the J 21 – had the engine, a licensed Daimler-Benz DB 605B, simply fitted at the rear of the main body, behind the cockpit and between the longitudinal booms. The jet version – J 21R – was fitted with air in-takes at both sides of the fuselage, having the engine (a De Havilland Goblin 2 and later a Swedish-licensed version, a Flygmotor RM1) located on the same area as the piston-propelled version and elongating the main body. The fuselage section harbouring the engine was also widened. Another modification was that the elevator was placed at the upper area of the double tail plane. The wing in both configurations was a low-wing, being straight until it met the longitudinal booms, changing into a slightly swept wing from the longitudinal boom to the wing tip. It also received wingtip fuel tanks.

The J 21 could develop speeds up to 645 km/h (400,78 mph), while the jet propelled version could develop speeds up to 800 km/h (497 mph), being a fast aircraft in both configurations. Its firepower (J 21) was equally powerful, as it was armed with a 20 mm cannon, either a Bofors or a Hispano-Suiza HS.404, and 2X 13,2mm Bofors machineguns at the nose, with 2X 13,2mm Bofors machineguns in the wings. The J 21R received an even much more considerable firepower, as it featured a 20mm Bofors cannon, 4X 13.2mm M/39A heavy machine guns, a centreline pod with 8X 13.2mm M/39 machineguns, and wing racks for 10X 100mm, 5X 180mm, or 10X 80mm anti-armour rockets.

Saab J 21 Prototype
Prototype in Service

The J 21 was initially developed with the aim of providing Sweden with good air assets to defend its air space and neutrality, and also with the aim of replacing many of the existing airplanes development. The development began in 1939, under the lead of Frid Wänström, having as basis a Bristol Taurus as an engine, yet it fell into a momentary freeze until 1941, when it was resumed. This freeze was due to Saab’s concentration in the Saab B 17 and B 18 bombers. As the configuration resulted problematic for the pilot’s safety when bailing out, many proposed solutions came, such as blowing the propeller, blowing the entire engine or using a “bomb crutch” to throw the pilot away from the airframe. The solution came with the development and implementation of a Bofors ejection seat, which was tested first on ground and in-flight on a SAAB B 17. The nose landing gear wheel was tested on a steel platform attaching the three undercarriage components, with the structure being towed by a truck during the test programme. In 1943 the first flight of the prototype took place, with units entering in service with the Flygvapnet in 1945. Three prototypes were built during the development process. In 1947 the J 21 evolved into de J 21R when it received the De Havilland Goblin jet engine, but as the J 29 Tunnan was introduced, it replaced the J 21 as the main fighter, performing the J 21 instead ground attack missions, thus designated A 21R.

The J 21 was in service with the Flygvapnet from 1945 until 1954, with 298 fighters built from 1945 to 1949. The J 21R was in service with the Flygvapnet from 1950 until 1956, with 60 units built from 1950 to 1952. Three J 21 are preserved as static displays in museums.

Design

Saab 21 R
The jet powered Saab 21 R in flight

The basic design of the J 21/J 21R was a twin-boom tail pusher propeller, making it one of the most radical operational designs of those times. This scheme proved to be beneficial for two important aspects. First, it benefited both pilot view forward and allowed the armament to be concentrated on the nose, meaning that such combination provided a good firing scope and sight, let alone a good firepower and making maintenance services rather easy. Second, it made possible for the aircraft to be updated thus being able to install a jet engine using the same airframe of the piston-propeller engine version, which was basically the basic airframe.

The only drawback of this layout – mainly with the J 21 piston-propelled engine version – was the risk for the pilot to hit the blades when bailing out, as the engine was placed right behind the cockpit. The solution came with one of the first ejection seats in the world, developed by Saab in 1943, being tested on the ground and on-flight and being a SAAB B 17 the testing platform. Another drawback was that, similar as the earlier versions of the Mustang P 51, the rearward view was rather poor, which could be problematic in a dog-fight. The J 21 featured a characteristic wing, as it was roughly strait from the main fuselage to the tail twin-booms, then being slightly swept back from the tail booms to the wingtips.

The wing was purposed with acquiring laminar flow as far as possible. In regards to the aerodynamics, it was required the airframe to reduce minimum drag and engine cooling drag, so the oil and liquid coolers, along with the duct system for the engine, inside the airfoil contour between the fuselage and the tail booms. Considering the tail boom design, the horizontal elevator was placed between the tail sections, connecting them. The landing gear, meanwhile, was of tricycle configuration and long, which made the J 21 to be a tall aircraft so to keep the propeller away from the ground. The rear gear retracted into the tail booms behind the rear wing spar, but this forced the fuel tank to be placed in the wing centre section. The frontal wheel was located at the nose.

The engine was a Daimler-Benz DB 605B inverted V12 of 1475 hp, which gave the airplane speeds of maximum 645 km/h (400,78 mph), but as the engines were received in poor conditions, improvements and overhauling were required. As a result of the power provided by this engine and the aerodynamic characteristics, the J 21 was deemed good, as it had excellent handling, benign stall characteristics and tight turning circle. The armament also gave this fighter good firing power, with the Swedish pilots being able to compare it with the Mustang P 51D (Sweden received a good number of them) and considering they were a good match for it. But the main drawbacks were that at medium and high altitudes performance tended to decrease, the rearward view was poor, and the controls were heavy to operate, increasing tiring during combat.

The armament of the J 21 consisted of a 20 mm cannon, either a Bofors or a Hispano-Suiza HS.404, and 2X 13,2mm Bofors machineguns at the nose, with 2X 13,2mm Bofors machineguns in the wings. The J 21A-3 was able of carrying unguided rockets (2X 180mm or 8X 80/145mm) and bombs (600kg, 500kg, 250kg or 4X 50Kg).

Saab 21 Cockpit

After World War II, the jet engine technology was becoming the mainstream propulsion system, and the Flygvapnet wanted to catch up and incorporate such technology into its assets. As the development of a new jet propelled fighter would take some time, the J 21 was chosen to be the platform for using an airframe in use with the new technologies back then. As a result, the J 21R was developed and introduced, with the first prototype taking flight in 1947 and then entering service in 1950. This ‘new’ fighter required some structural changes so to cope with the new power plant, like up to 50% of its airframe. First, the main body was slightly prolonged ant widened, so to allow the De Havilland Goblin 2/Flygmotor RM1 engine (that allowed speeds of 800 km/h) and the air intakes, located at each side of the fuselage. In addition, the stabilizer was moved upwards top to the fin, so to allow the engine flow, requiring the tails to be redesigned. The wing leading edge was mover forward and made sharper. Airbrakes were introduced, one upward and other downward flaps placed on the outer wing’s trailing edge. Given the increased speed, the ejection seats were properly modified so to enable ejections at subsonic speeds. And as the propeller was removed, the landing gear was shortened in turn, reducing the height of the airplane. Fuel tanks were fitted in the middle wing and the wingtips, which increased the fuel volume.

The J 21R received an enhanced firing power, as the standard 20mm cannon/4X 13,2mm M/39A heavy machineguns set was added with a centreline external pod carrying 8 additional 13,2mm M/39 heavy machineguns. In addition, the J 21R was fitted with wing racks allowing the airplane to carry 10X 100mm or 5X 180 Bofors rockets, or 10X 80mm anti-armour rockets.

Materializing ‘Armed Neutrality’

The J 21 is, like the J 29 Tunnan, the product of Sweden’s concerns about its own security during WWII, especially in the light of Germany’s invasions of Norway and Denmark in 1940, which were neutral nations by the time. As Sweden considered that its existing air assets wouldn’t be able to successfully contribute to the defence, given their obsolete condition, it considered that new aircraft were necessary. As with the J 29, Sweden faced some problems when trying to acquire some technology due to the restrictions imposed by the conflict, although by sheer luck it was able to receive the Daimler-Benz DB 605B engine, as Germany was trying to hamper the delivery. These circumstances decided the Swedish government to undertake a local rearmament programme and implement a policy of ‘armed neutrality’ to secure the nation’s neutrality. The focus was placed on the development and fabrication of advanced aircraft. As the same concerns prevailed after World War II and into the very earlier days of the Cold War, it was deemed that the resulting technologies from the War needed to be exploited and incorporated, having in mind Sweden to catch up with the newly developed technologies, especially in regards of propulsion. The Saab J 21 became the platform for the Flygvapnet to make the transition from piston-propeller engine to jet engine, while at the same time providing the country with a locally built jet engine fighter, while newer and more advanced aircraft were put into service.

A feat of Swedish Nytänkande

The fact that the J 21 was used as a basis for an almost new jet powered engine fighter is a product of Sweden’s innovative thinking and also of its capacities – out of need, in part – of working with existing resources at the point of maximizing them. While the J 29 Tunnan has the honour of being the first jet fighter exclusively built for that purpose, it is the J 21 the very first jet engine fighter the Flygvapnet operated with, being amongst the very few designs, if not the only one, in being successfully modified as it received two different types of power plants. And while the J 29 Tunnan displaced the J 21 as a fighter, it was able to operate as a good ground attack aircraft until 1956, making this airplane born in the World War II, an early Cold Warrior and the basis for Sweden’s jet fighter industry and operationalization. It simply meant a huge step for the Swedish Air Industry, let alone its Air Force.

Variants of the J 21

  • J 21A-1 – Fighter version and the very first production series of the J 21. It featured the armament configuration of the 20mm Hispano-Suiza HS.404 cannon and the 13,2mm Bofors/Colt heavy machine guns. In service until 1949. 54 delivered.
  • J 21A-2 – Fighter version and the second and third production series, featuring enhanced avionics and incorporating a Bofors 20mm gun, with the other armament being the same. It was also equipped with further direction horizon instruments. In service until 1953-1954. 124 delivered.
  • J/A 21A-3 – Fighter/fighter-bomber version based from modified J 21A-2 airframes. It was equipped with a SAAB BT9 bomb aiming sight and two RATO (Rocket-Assisted Take-off) devices, armed with unguided rockets (2X 180mm or 8X 80/145mm) and bombs (600kg, 500kg, 250kg or 4X 50Kg). 119 delivered.
  • J 21B – A planned version to be armed with 3X 20mm guns at the nose, a radar in the starboard room, improved aerodynamics and better engines (A Daimler-Benz DB 605E/Rolls-Royce Griffon). It was also intended to feature a pressurized cockpit and a bubble canopy. Cancelled

Variants of the J 21R

  • J 21RA / A 21RA – First production series powered by a De Havilland Goblin engine. Later reconfigured into ground attack airplanes (A 21RA). Fitted with wingtip fuel tanks to increase the operational range and endurance. Operated until 1953. 30 delivered.
  • J 21RB / A 21RB – Second production series powered by a Swedish-license made De Havilland Goblin (RM1). It was also reconfigured later into a ground attack airplane (A 21RB), with the nose heavy machineguns changed to a 12.7mm caliber. Fitted with wingtip fuel tanks to increase the operational range and endurance. Operated until 1956. 30 delivered.

Operators

  • Sweden -The Flygvapnet operated the J21 a time roughly after the end of World War II. It operated with 54 fighters of the J 21A-1 version, 124 The J 21 fighters of the J 21A-2 version, and 119 fighter/bombers of the J 21A-3 version. The J 21 was in service between 1945 and 1954, with X units: F9 Goteborg, F15 Soderhamn, F12 Kalmar, F6 Karlsborg and F7 Såtenäs. In addition, the Flygvapnet operated with 30 fighters of the J 21RA version, and 30 fighters of the J 21RB version. Both were later on modified into ground attack airplanes, being denominated as a result A 21RA and A 21RB. The J 21R was in service from 1950 to 1956, with three units: The F10 Ängelholm, the F7 Såtenäs, and the F17 Kallinge. Three J 21 remain today as museum exhibitions in Sweden.

 

 

21 Specifications
Wingspan  11,6 m / 38 ft 0 in
Length  10,44 m / 34 ft 3,02 in
Height  3,97 m / 13 ft 0 in
Wing Area  22.2 m² / 238,87 ft²
Engine  1 Daimler-Benz (SFA) DB 605B inverted V12 of 1475 hp
Maximum Take-Off Weight  4431 Kg / 9,768.6 lb
Empty Weight  3250 kg / 7,165 lb
Loaded Weight  4150 kg / 9,149 lb
Maximum Speed  645 km/h / 400,78 mph
Range  750 Km / 466 miles
Maximum Service Ceiling  11000 m /36,090 ft
Climb Rate  15 m/s (2,950 ft/min)
Crew 1 (pilot)
Armament
  • 1 X 20 mm Hispano-Suiza HS.404 or a Bofors cannon located at the nose.
  • 2 X 13,2 mm Bofors (Colt) heavy machine guns located at the nose.
  • 2 X 13,2 mm Bofors (Colt) heavy machine guns located at the wings.
  • The J 21A-3 fighter/bomber version could carry also 2 X 180mm, or 8X 80/145mm rockets; and 600kg, 500kg, 250kg or 4X 50Kg bombs

 

21R Specifications
Wingspan  11,37 m / 37 ft 4 in
Length  10,45 m / 34 ft 3 in
Height  2,90 m / 9 ft 8 in
Wing Area  22.3 m² / 260,0 ft²
Engine  1 De Havilland Goblin 2 Turbojet (Svenska Flygmotor RM2B Turbojet)
Maximum Take-Off Weight  5000 Kg / 1,0230 lb
Empty Weight  3200 kg / 7,055 lb
Loaded Weight  N/A
Maximum Speed  800 km/h / 497 mph
Range  720 Km / 450 miles
Maximum Service Ceiling  12000 m /39,400 ft
Climb Rate  17.1 m/s (3,366.1 ft/min)
Crew  1 (pilot)
Armament
  • 1 X 20 mm Bofors cannon located at the nose.
  • 4 X 13,2 mm M/39 heavy machine guns located at the nose, later changed to 12.7mm caliber.
  • 8 X 13,2 mm M/39 heavy machine guns on a centreline pod.
  • Wing racks allowing 10X 100mm, 5X 180mm, or 10X 80mm anti-armour rockets.

Gallery

Saab J 21A-1 - Prototype
Saab J 21A-1 – Prototype
Saab A 21A-3 - 21364
Saab A 21A-3 – 21364
J 21R - Prototype
Saab J 21R – Prototype
Saab A 21R Trainer - 21455 Side Profile View
Saab A 21R Trainer – 21455
Saab J 21R - 21463 w/ Gun Pod Side Profile View
Saab J 21R – 21463 w/ Gun Pod

Saab A 21A-3 Converted J21R Converted J21R 2

Saab 21 R
The jet powered Saab 21 R in flight
Saab J 21 in Service
Saab J 21 in Service
Saab J 21 Prototype
Prototype in Service
Saab J 21A-3 in a Hangar
Saab J 21A-3
Saab 21 Cockpit
Saab 21 Cockpit
Saab 21R - Flightline
Saab 21R – Flightline

Sources

Chant, C. (2001). Aviones de la Segunda Guerra Mundial [Aircraft of World War II, Fabian Remo Tamayo & Fernando Tamayo, trans.]. Madrid, Spain: Editorial LIBSA, Sharpe, M. (2001). Jets de Ataque y Defensa [Attack and Interceptor Jets, Macarena Rojo, trans.]. Madrid, Spain: Editorial LIBSA, Goebel, G. (2014). The SAAB J 21 & J 21R. Air Vectors., Frederiksson, U. (2000). Saab J 21/A 21/A 21R. x-plane.org,  Aviastar.org (n.d.). Aircraft Profile #138. Saab J.21A & R., Aviastar.org (n.d.). Saab 21R. 1947., NGO valka.cz. (2015). Saab J 21R., Saab. (n.d.). 1940’s., SAAB 21. (2016, June 23). In Wikipedia, The Free Encyclopedia., Saab 21R. (2016, June 8). In Wikipedia, The Free Encyclopedia., Images: Converted J 21R, Converted J 21R 2, Saab A 21A-3 – Alan Wilson / CC BY-SA 2.0, Side Profile Views by Ed Jackson – Artbyedo.com

Saab J 29A Tunnan - 29606 Side Profile View

Saab 29 Tunnan

Cold War, Sweden, , ,

sweden flag Sweden (1950)
Fighter Plane – 662 Built

The Saab 29 Tunnan was a single-seat, single-engine transonic aircraft and first-generation jet fighter. It was a small aircraft with a single central air intake placed at the nose, a bubble cockpit and  thin sweptback wings. It was the very first Western European design to have a swept wing layout of 25 degrees rearward, incorporating many of the latest technologies of the time. Saab obtained access to WWII German studies involving swept wings and their positive effects in regards to speed in Switzerland, and as a result, the J 29 Tunnan came to be similar to the German Luftwaffe’s Messerschmitt Me P1101 project.

Nazi P.1101 vs Saab Tunnan

The Tunnan acheived a top speed of 1035 km/h which made it one of the fastest aircraft in the world in 1950. The nickname: ‘Flying Barrel’ was coined due to the shape of the fuselage, which came to resemble the shape of a barrel due to the large cross section of the engine and the size of the engine itself with a tapered nose and aft section. The Tunnan’s ungainly and small appearance could be deceiving  however it was fast enough to set several world speed records and also had a very good agility. However, the aircraft proved challenging for inexperienced pilots. The 29 was comparable to its contemporaries: the US-made F-86 Sabre and the Soviet-made Mig-15.

The development aimed initially at producing a fighter-interceptor, but reconnaissance and ground attack versions were also developed and produced, however a training version was not produced due to time constraints of the production schedule. Sweden was developing a strong air defence system that enabled it to take advantage of innovations introduced in WWII. As a result, by late 1945 the development of the Tunnan began, with the Swedish Royal University of Technology and the National Aeronautical Research Institute taking part by providing wind tunnel testing that defined the general aerodynamics of the Tunnan. Just like the Saab J32 Lansen, a single Saab Safir was modified, fitting swept wings to its airframe in order to test the design of the wings alone.

Four prototypes were built during the development process, with the first two lacking any sort of weaponry carrying heavy testing equipment instead, and the third prototype carrying four 20mm Hispano Mark V cannons. These prototypes tested different aerodynamic features, such as the location of the airbrakes – either in the fuselage or on the wings, as well as the configuration of the ailerons and flaps. The prototypes also hinted that the Tunnan design would be able to reach and even exceed the maximum Mach they were designed for. Once in service the Tunnan broke many records. It set a world speed record on a 500 km closed circuit as it reached a speed of 977 km/h in 1954. The reconnaissance version set also a record of 900.6 km/h in a closed circuit of 1000 km.

In 1948, the J 29 Tunnan flew for the first time, in service with the Flygvapnet from 1951 until 1976, with 662 fighters built from 1950 to 1956 making the Tunnan the most numerous aircraft produced Saab, as well as the longest lived design in service. It also served with the Austrian Air Force with 30 units in service until 1973. A single J 29F still can be seen flying at airshows around Europe.

Design

The Tunnan is a thin 25 degrees swept back laminar-flow mid-wing fighter, having a single tail and a single engine, featuring the design similar to most of the first generation jet fighters: a single engine with a central straight-through airflow system that maximized thrust. Two tubular pitot sensors were located at the wing tips. For lateral stability during take-off and landing, automatic-locking leading edge slots were fitted in the wings and were also interconnected with the flaps. It was later on enhanced with the installation of an afterburner and of dog-tooth leading edge in the wings – which increased the Mach speed the Tunnan could attain. Trim tabs and dive brakes were also incorporated to the design, being initially placed on the wings and later re-located to the fuselage, directly forward of the main landing doors.

The Tunnan also featured a bubble shaped canopy with the cockpit located right above the engine air intake, and forward the wing’s leading edge. The canopy was opened by sliding backwards, allowing the pilot to access and exit. The design also took advantage of the already existing ejector seat developed in 1943 by Saab, complemented by an explosive jettison system to remove the canopy in case of ejection. The landing gear was of tricycle configuration, with the rear wheels retracting into the fuselage, which contributed in making the wings thin, and a single wheel gear at the nose. The vertical stabilizer had a tapered edge, being straight trailing edge with a blunt tip, with the tail section placed above and behind the engine exhaust nozzle. In turn, the horizontal stabilizer is mounted practically at the base of the tail. The Tunnan proved to be not only a very capable and agile fighter, but also proved very durable in sorties. During a UN mission in the Congo it received intensive ground fire without sustaining any noticeable damage.

The engine, along with its aerodynamic characteristics, made of the Tunnan a fast fighter. The powerplant consisted of a DeHavilland Ghost turbojet engine producing 5000 lbs of thrust. This engine was deemed suitable for the fuselage of the Tunnan, replacing the originally planned DeHavilland Goblin, and had the advantage of making maintenance easy with the engine cowling able to be removed as a single piece.

The armament of the Tunnan consisted of four 20mm Hispano Mark V cannons placed in pairs on both sides under the nose. The pylons were capable of carrying 75mm air-to-air rockets, 145mm anti-armour rockets, 150mm HE (High Explosive) rockets and/or 180mm HE anti-ship rockets. Later versions were capable of using Rb24/AIM-9 Sidewinder air-to-air missiles. Fuel air-drop tanks could be used as napalm bombs.

Swedish Resolve

Tunnan Banking Maneuver
Tunnan Banking Maneuver

The Tunnan is the product of Swedish concerns about its security during World War II, in the face of Germany’s rapid annexations of both Norway and Denmark and acknowledging the country was unable to resist such aggression. But there were also of concerns that Sweden was falling behind after the rapid development of technologies and innovations brought about during the war. Sweden’s isolation in this aspect was exacerbated by the degree of defense secrecy by both the Axis and Allied countries. As a result, an effort was made in order to strengthen defensive capabilities with the focus being placed on the development of modern aircraft to bolster air defence, exploiting the war-time innovations in power – namely the recently introduced jet propulsion technologies as well as other advances in aircraft design. The new technologies were exploited after Sweden obtained access to research after the war. The already existing Saab J 21R was utilized to make the transition between the piston and jet propelling engines and to provide a temporary solution, but it was deemed necessary to develop a much more modern aircraft in order to keep the air defences fit. The Tunnan became the solution, making the Swedish Air Force the 4th largest during the mid-century.

Peacemaker from the North

All the aircraft produced by Saab and in service with the Flygvapnet from 1948 to 1989 saw relatively little combat. The Tunnan constitutes the only exception, as it saw extensive use during conflict in Central Africa. As the crisis in the Congo unfolded in 1961, Sweden contributed five J29B Tunnans that were tasked with protecting UN’s air transport and providing fire support to cover UN ground troops when needed, constituting the F22 unit. In 1962, four additional J29Bs and two J29Cs were sent. The 11 Tunnans provided by Sweden to the UN mission comprised the only air component of the UN at the time. As the crisis evolved and the additional six Tunnan were required, air superiority was achieved along with ground attack missions that involved the utilization of the fighter’s 4 Hispano cannons and rockets. The missions mainly focused attacks on military trains and airfields at Katanga, as other aerial assets from Ethiopia – F 86 Sabres – and India – Canberra light bombers – withdrew. When the UN peacekeeping mission was over in 1963, four of the Tunnans returned to Sweden, while the remaining met an ignominious ending, destroyed at the base, as it was deemed prohibitively expensive to return them.

Variants

  • J 29 – Four prototypes built in 1948-1950, for the development process only.
  • J 29A – Fighter version. Armed with four 20mm Hispano Mark V cannons, and 12 75mm anti-armor rockets. Later series relocated the wing-mounted dive brakes into the fuselage. Remained in service until 1965. 224 delivered.
  • J/A 29B – Fighter/attacker version. It featured an increased 50% fuel capacity and wing hardpoints with provisions to carry bombs, rockets – 8 or 14 80mm or 145mm anti-armour; 8 or 14 150mm HE; 2 or 4 180mm anti-ship – and fuel drop-tanks that could be used as napalm bombs. Served until 1965. 332 delivered.
  • J 29C – Reconnaissance version for day and night operations. It carried between 5-6 cameras in a modified nose, being unarmed cameras replaced the 4 guns. It received the same wing enhancement of the J 29E. It also became the first jet-powered photographic-reconnaissance aircraft introduced by a non-aligned nation, as well as the first Swedish aircraft to be equipped with radar warning receivers. An antenna for backwards-looking radar was placed at the tail cone, being afterwards relocated  This version set a new speed record back in 1955, reaching speeds 900.6 km/h (559.6 mph) in a closed circuit of 1000 kms (621.4 miles). 76 delivered.
  • J 29D – A single unit to test the DeHavilland Ghost RM2 turbojet fitted with an afterburning thrust, later upgraded to J 29F.
  • J 29E – Fighter version, which incorporated an enhanced wing design by fitting leading edge dogtooth, aimed at increasing critical Mach number. It also increased load factor. Same armament configuration as the J 29B. Upgraded to the J 29F version. 29 delivered.
  • J 29F – Fighter version, which were modified J 29B and J 29E airframes. This version featured the enhanced wing design of the J 29E, and the DeHavilland Ghost engine equipped with an afterburner. This version was also optimized to carry two Saab Rb24 (AIM-9 Sidewinder) missiles in 1963, having the same armament payload of the J 29B. It also performed in the role of aggressors, and performed target towing. Most were retired by 1967. 308 converted aircraft.
  • SK 29 – Planned training version. It could have featured a two-seated cockpit, with seats placed side-by-side, no armament and limited fuel capacity. Cancelled.
  • J 29R – All-weather fighter version equipped with an air intercept radar. Cancelled.

Operators

  • Sweden – The Flygvapnet operated the Tunnan from 1951 to 1967, having 665 units operating, all of the J 29A, J/A 28B, J 29C, J 29E and J 29F versions. Some were kept for countermeasures trainers and target towing duties until 1976. 11 J 29Bs and J 29Cs took part in the United Nations Operation in the Congo (ONUC), being the only Tunnan, and actually the only aircraft during the Cold War of the Swedish Air Force to take part in combat operations abroad.
  • Austria – The Österreichische Luftstreitkräfte (Austrian Air Force) operated 15 restored J 29Fs by Saab in 1961, where they formed the first Jagdbomber Staffel. An additional 15 restored J 29Fs were sold to Austria, where the two guns on the port side could be replaced by three cameras, which were moveable during flight forming the second Jagdbomber Staffel in the Austrian Air Force. These remained in service until 1972.

 

J 29F Tunnan Specifications
Wingspan 11 m / 36 ft 1 in
Length 10.23 m / 33 ft 6.7 in
Height 3.75 m / 12 ft 3.6 in
Wing Area 24.15 m² / 260 ft²
Engine 1 DeHavilland Ghost 50 Turbojet (Svenska Flygmotor RM2B Turbojet)
Maximum Take-Off Weight 7,530 kg / 16,600 lb
Empty Weight 4,580 kg / 10,097 lb
Loaded Weight 13,529 kg / 35,273 lb
Maximum Speed 1,035 kmh / 643 mph (1,075 kmh / 668 mph in full afterburner)
Range 1,500 Km / 932 miles
Maximum Service Ceiling 13,700 m / 45,000 ft
Climb Rate 2,400 m/min (7,874 ft/min)
Crew 1 (pilot)
Armament
  • 4 X 20 mm Hispano Mark V located at the nose
  • 2 Saab Rb 24 (AIM-9 sidewinder) missiles
  • 75mm air-to-air rockets
  • 80mm or 145mm anti-armour rockets, 150mm HE rockets, and/or 180mm HE anti-ship rockets.
  • 4 X SKa 10 cameras, 1 X SKa 15 camera for mapping, and 1 X SKa 5.
  • 2 X fuel drop tanks that could be used as napalm bombs.

Gallery

Saab J 29A Tunnan - 29606 Side Profile View
Saab J 29A Tunnan – 29606
Saab J 29A Tunnan - 29670 Side Profile View
Saab J 29A Tunnan – 29670
Saab S 29C Tunnan - Congo Conflict of 1961 Side Profile View
Saab S 29C Tunnan – Congo Conflict of 1961
Tunnan Landing Gear
Tunnan Landing Gear
Tunnan Front View
Tunnan – Front View
Tunnan Afterburner
Tunnan Afterburner
Tunnan Banking Maneuver
Tunnan Banking Maneuver
Tunnan Taxiing
Saab J29 Tunnan – 29670
S 29C Tunnan in UN service in 1961
S 29C Tunnan in UN service in 1961
Nazi P.1101 vs Saab Tunnan
The P.1101 of Nazi Germany compared with Saab’s Tunnan a few years later



Sources

Ängelholms Flygmuseum (n.d.). Flygplan J29 Tunnan Historia., Aviastar.org (n.d.). Aircraft Profile #36. Saab J.29., DefenceViewpoints. (2015). Five generations of US jet fighters., Dorn, W. (2013). The UN’s First “Air Force”: Peacekeepers in Combat, Congo 1960 – 1964., Goebel, G. (2016). The SAAB 29 Tunnan & SAAB 32 Lansen. Air Vectors., Guttmann, J (1998). Defining the Jet. HistoryNet., Henriksson, L. (2010). J 29 – SAAB “Flygande Tunnan” (1951-1979)., Johnson, D. (2010). Messerschmitt Me P.1101. Luft46.com., Liander, P. (2002). För 50 år sedan… J 29 Tunnan gör entré. FlygvapenNytt, (2), 34-35, Saab. (2014). J-29 Tunnan in UN Service., Saab. (2015). J-29 Tunnan Fighter, Attack and Surveillance Aircraft., Saab. (n.d.). 1940’s., Wagner, P. J. (2009). Air Force Tac Recce Aircraft. Pittsburgh, Pennsylvania: RoseDog Books., Werner, B. (2011). J29 Tunnan, Saab., Saab 29 Tunnan. (2016, July 16). In Wikipedia, The Free Encyclopedia. Images: Tunnan-29670-1997 by Rob Schleiffert / CC BY-SA 2.0, Tunnan Underside + Tunnan Gear by Alan Wilson / CC BY-SA 2.0, Tunnan Taxiing by Anemone Nemorosa / CC BY 2.0, Tunnan Afterburner by SteveH1972 / CC BY-ND 2.0

 

Saab Lansen J32D - 32606 Side Profile View

Saab 32 Lansen

Cold War, Sweden, , ,

sweden flag Sweden (1952)
Fighter Plane – 452 Built

A tandem two-seat, single-engine transonic aircraft. Intended initially as an attack aircraft, it was later developed into fighter, reconnaissance, and ECM versions thanks to the aircraft’s size, which allowed the development of the aforementioned variants. The aircraft also had low swept back wings and similar elevators located on the tail. Developed in order to replace the WWII-era light bombers, attack and reconnaissance Saab B 18/S 18, the Saab J 21R/A 21R, and provide a ground-attack complement to the Saab J 29 Tunnan. It was also developed after Flygvapnet requested an aircraft capable of attacking anywhere along Swedish long coastline within one hour after taking off from a central location, and to be capable of operating in any weather conditions, and in both day and night.

Development of the Lansen

Saab J32D Lansen - 32606

Lansen development began by 1946 with the project P1150, where a configuration of two engines was at first considered but latter scrapped given many accidents with foreign aircraft having such display. A Saab 91 Safir, a piston/propeller engine training light aircraft was modified by incorporating the swept back wings intended for the Lansen, in order to test the design. Its first flight took place in 1952, being a very advanced concept in both design and configuration, as it was an aircraft with the best design and quality in comparison to any other European design of the times. In fact, it is among the first designs in incorporating a radar. Another interesting fact is that the Lansen was the first aircraft to be designed upon a mathematical coordinate system, instead of blue prints. It also broke the sound barrier in 1953, as it exceeded Mach 1 while performing a shallow dive. In 1956 it entered in service with the Flygvapnet. 452 aircraft were built between 1954 and 1960, remaining in service until 1997, although three Lansen with experimental, research and test and trial tasks were still operating as of 2012.

Design

Saab Lansen and Hawker Hunter in Formation
Saab Lansen and Hawker Hunter

The Lansen is designed as a swept back low-wing fighter, with a single tail and a single engine, a Volvo Svenska Flygmotor RM6A, enabling a maximum speed of 1123 km/h. The Lansen was among the first aircraft to be built specifically for attack missions. Its airframe was a sleek, streamlined and clean design, in which every line was calculated using a mathematical early computer-based design. It could sustain +12g and -8g. Its low wings had a 35° sweep and a composition of up to a 10° laminar profile, having hydraulically-boosted ailerons. One-section stall fences were installed on the wings, a pitot tube on the right wing and three hardpoints. The landing gear was of tricycle configuration.

The engine was originally intended to be the Swedish STAL Dovern RM4, but as it was not ready by the time the prototypes were completed. The Svenska Flygmotor RM6A, a Swedish version of the Rolls-Royce Avon, was the used in the Lansen. The afterburner was of Swedish design. The air intakes for the engine were located at both sides of the fuselage, forward of the wing root and cockpit.

Radar

The Lansen is among those first designs implementing onboard radar. The radar array was a PS-431/A based on the French design that worked in coordination with the anti-ship Rb04C missile, one of the first “fire and forget” missiles. As not all the squadrons were equipped with radar, and usually only one aircraft of the group would carry a navigator, the Lansen  equipped with both radar and a navigator would be the leader of the group guiding the other aircraft to the target. The radar would work in tandem with a Saab S6 computerized fire-control system, a Hughes AN/AAR-4 infrared search & trach (IRST) sensor, with the radar gunsight indicating to the pilot when there would be an optimal firing solution (these systems were mostly equipped in the J32B). The S32C was equipped with a radar warning receiver, and the J 32E was equipped with jamming devices instead of the radar in the nose. All aircraft were equipped with Saab ejection seats for the crew.

Weaponry

An RB-04 Anti Ship Missile equipped on an A32A
An RB-04 Anti Ship Missile equipped on an A32A

The Lansen would carry a varied array of weaponry depending on mission and version. The basic weapons were 4 X 20 mm Bofors (or Aden M/55 30 mm) guns located at the nose, 2 Saab 304/Rb 04 anti-ship missiles or 12 or 24 unguided rockets (60, 63, 75, 135, 145 and 180 mm), and up to 12 iron-bombs (15, 50, 80, 120, 250, 500, 600 kg). it could also carry 4 Rb 24 AIM Sidewinder missiles, ECM pods, target towing pods, jamming equipment, cameras, and chaff dispensers.

A Versatile Advanced Aircraft and Potential Nuclear Warrior

Saab J32E - 32512
Saab Lansen J32E – 32512

The Lansen was a large airframe providing a versatile platform to carry a variety of different arms depending up on mission.  Along with the Saab AJ 37 Viggen, the Lansen was a contender to carry nuclear weapons as a deterrent to protect the region, but ended up never being utilized in this role. It would have been interesting to see how a nuclear-armed version of the Lansen might have worked. But even if the Lansen in the end was not a nuclear warrior, it could boast of having a very advanced capability thanks to its design process, which was the first to be designed using a computer. Furthermore, it is among the first post-war designs to have incorporated its own radar, in addition to being among the first operational swept back wing designs.

Variants

  • A 32A – The ground attack and maritime strike version of the Lansen, and the basic one. Armed with four Bofors 20mm guns on the nose, with a special device to deflect the empty casing from entering the air intakes. The fuel tank nose was also protected with a neoprene cover to protect from the casings impact. The aircraft could also carry one of the first “fire and forget” missiles, the anti-ship Rb04/Saab 304 missile. It could also carry bombs and rockets of varied calibres and payload. This version was intended to carry the nuclear weapons developed by Sweden, should it nuclear programme was not cancelled by the 60’s. Remained in service until 1978. 287 delivered.
  • J 32B – All-weather fighter version, mainly used in adverse climate conditions and at night. Armed with four 30mm Aden cannons with the casing being retained, sparing the protective measure implemented on the J 32A. 4 Air to air Rb24/ AIM 9 Sidewinder missiles and 75 m/57 mm rockets were also part of this version’s armament, all being fired by radar sighting. There was a radar display for the pilot and not exclusively for the navigator, allowing targeting without visual thanks to the fitted IR sensor (AN/AAR-4) on the wing. Remained in service until 1973. 118 delivered.
  • S 32C – Maritime surveillance and photo reconnaissance version. Fitted with a PS-432/A radar with longer instrumented range, and four cameras (SKa 17 and SKa 18), latter, SKa 23, SKa 15 and Jugner FL S2 cameras were fitted. All the cameras were for low, high and night takes. Twelve additional British 75 kg photo flash bombs were also used, mainly on the wings. Chaff dispensers and RWR gear – to give visual and aerial warning – were installed. In service until 1978. 44-45 delivered.
  • J 32D – Target towing version modified from six J 32B airframes. Remained in service until 1997. 6 delivered.
  • J 32E – ECM version from modified 15 J 32B. Also tasked with ECM warfare and ECM training. The radar was replaced by a G24 radar-jamming device against ship and land-based radars, and two chaff dispenser were incorporated. It also carried 120kg dummy bombs.  Remained in service until 1997. 15 delivered.
  • J 32AD – A proposed daytime fighter version purposed to replace the J29 Tunnan. It would have been a single seat fighter with four 20 mm guns and a fifth 30 mm gun, all located on the nose. It would have been armed also with rockets and missile but lacking a radar. Never developed and instead 120 Hawker Hunters entered in service, filling the gap between the J 29 Tunnan and the J 35 Draken.
  • J 32U – Another proposed fighter version with enhanced performance than the J 32B, with a Rolls-Royce RA 19R engine, a supplementary rocket engine, a thinner wing with 40° of sweepback, and a flying tail. Political decisions and considerations of replacing the Lansen with other types of aircraft after 8 years of service prevented this development to see the light.

Operators

  • Sweden – The Flygvapnet was the only operator of the Lansen, having this aircraft in service from 1956 to 1997. 118 airframes where of the J 32A version; 118 airframes where of the J 32B version – 6 were modified to the J 32D and other 15 were modified to the J 32E versions – and 44-45 airframes where of the S 32C version. 452 J 32 Lansen served in total with the Flygvapnet until 1997. Three Lansen remained in service by 2012 with experimental and research purposes.

 

Lansen Specifications
Wingspan 13 m / 42 ft 7 in
Length 14.94 m / 49 ft 0 in
Height 4.65 m / 15 ft 3 in
Wing Area 37 m² / 529,8 ft²
Engine 1 Svenska Flygmotor (Rolls-Royce Avon) turbofan RM6A
Maximum Take-Off Weight 13,600 Kg / 29,982 lb
Empty Weight 7,438 kg / 16,397 lb
Loaded Weight 13,529 kg / 35,273 lb
Maximum Speed 1,125 km/h / 699 mph
Range 3,200 Km / 1,988 miles
Maximum Service Ceiling 16,000 m /52,493 ft
Climb Rate 60 m/s (11,811 ft/min)
Crew 2 (pilot & navigator)
Armament
  • 4 X 20 mm Bofors or Aden0 M/55 30 mm guns located at the nose.
  • 2 Saab 304/Rb 04 anti-ship missiles.
  • 12 or 24 unguided rockets (60, 63, 75, 135, 145 and 180 mm).
  • Up to 12 iron-bombs (15, 50, 80, 120, 250, 500, 600 kg). It could have also carried nuclear bombs, in case Sweden would have continued its nuclear programme.
  • 4 Rb 24 AIM Sidewinder missiles.
  • ECM pods, target towing pods, jamming equipment, cameras, and chaff dispensers

Gallery

Saab J32E Lansen - 32620 - Side Profile View
Saab J32E Lansen – 32620
Saab J32E Lansen - 32512 - Side Profile View
Saab J32E Lansen – 32512
Saab J32E Lansen - 32507 Side Profile View
Saab J32E Lansen – 32507
Saab Lansen J32D - 32606 Side Profile View
Saab Lansen J32D – 32606
Saab J32 Banking Maneuver
Lansen Banking Maneuver
An RB-04 Anti Ship Missile equipped on an A32A
An RB-04 Anti Ship Missile equipped on an A32A
Saab J32D Lansen - 32606
One of many still airworthy Lansens enjoying retirement at an airshow.
Saab J32E Lansen equipped for ECM
Saab J32E Lansen
Saab Lansen and Hawker Hunter in Formation
Saab Lansen and Hawker Hunter
Saab J32E - 32512
Saab Lansen J32E – 32512


Sources

Aguilera, R. D. (2015). Saab 32 Lansen, Bergmans, W. (2011). J32 Lansen, Saab, Fortier, R (1997). Photo Essay Collection. Shield and Sword: Fighter Aircraft Development in the 1950s. Ottawa, Canada: National Aviation Museum., Globalsecurity.org (2012). Swedish Nuclear Weapons., Goebel, G (n.d.) The Saab 29 Tunnan & Saab 32 Lansen., Jackson, R. (2010). 101 Great Fighters. New York, NY: Rosen Publishing., Saab (2015). Saab 32 Lansen., Saab (n.d.) 1950’s.,  Sharpe, M (2001). Jets de Ataque y Defensa [Attack and Interceptor Jets, Macarena Rojo, trans.]. Madrid, Spain: Editorial LIBSA, WarbirdsUpdate (2013). The Swedish Air Force Historic Flight from Within the Cockpit. Warbirds News., Saab 32 Lansen. (2016, June 12). In Wikipedia, The Free Encyclopedia., X-Plane.org (2008). Dispersed Basing. X-Plane.org. Images: Saab Lansen 32606 by MrTMan / CC BY-SA 2.0, Saab Lansen 32512, Lansen & Hunter by Alan Wilson / CC BY-SA 2.0, Saab J32E Lansen by Leonid Kruzhkov / CC BY-ND 2.0,  RB-04 Anti-Ship Missile by AdurianJ / CC BY 2.0, Plane Profile Views by Ed Jackson

 

Saab J35J Draken - 35556 - Side Profile View

Saab 35 Draken

Cold War, Sweden, , , ,

sweden flag Sweden (1960)
Fighter Plane – 651 Built

A single-seat, single-engine interceptor/fighter for all-weather conditions, with low double delta wings, the Saab 35 Draken was developed in order to replace the Saab J29 Tunnan and the Saab J32 Lansen. Its first flight took place in 1955, being amongst the most advanced and remarkable fighters of its time. In 1960 it entered in service with the Flygvapnet.

Development of the Draken

Draken development started in 1949, following a requirement by the Flygvapnet for a single-seat cost-efficient interceptor with supersonic capabilities and high climbing rates, able to operate in short airstrips – or even highways, roads and unprepared runways – and easy to operate with high adaptability. As a result of both the requirements and development process, the result was a double-delta winged fighter that became the first European supersonic fighter, and also a high performance air-defence asset for Sweden. And on a similar fashion as the JAS 39 Gripen and JAS 37 Viggen, it was required the Draken to be serviced, refuelled and armed up to ten minutes by untrained ground personnel. A brake parachute was incorporated to reduce landing distance. Interestingly, a prototype was built expressly to test the double-delta wing concept: such was the Saab 210 ‘LilDraken’.

J35J in Flight - Swedish Air Force
J35J in Flight – Swedish Air Force

The Draken is also a product of the needs from a neutral nation willing to keep its neutrality, and geographically placed between the two block. This reason explains the requirements, but especially its high climbing rate capabilities, so to be able to engage high-altitude bombers and fighters – namely Soviet Union bombers and fighters. It also explains the need for STOL capacities, as the Flygvapnet was implementing a system of dispersed bases, asking for highways and roads to be used as airstrips from where the aircraft could be operating, and also to reduce damage and increase survival in case of attack.

Its very unique and remarkable double-delta wing design is also explained by the technical abovementioned requirements, which gave the aircraft very good high and low speed performances. This design made the Draken capable of executing the “Cobra” manoeuvre, and also to stand well against more recent designs, as air exercises in Austria evidenced. During development it was able to unintendedly exceed Mach 1 on its first afterburner flight. It could also sustain a force of 10G turning force. And it also had a safety feature, with the introduction of a ram turbine, placed under the nose, to provide emergency power.

Despite being conceptualized as an interceptor, it performed well in dogfights and was able to undertake ground attack, training, and reconnaissance missions as well. And it proved to be a very tough and resistant design, as it is among the few jet fighter designs to be in service for 50 years. Austria, Denmark, Finland, Sweden and US National Test Pilot School were the operators of the Draken.

The design was so unique that, in fact, the Draken was studied for the design and development of the F16XL experimental prototype.

Between 600 and 650 Draken were built, serving with the Flygvapnet until 1998, with the Finnish air force until the year 2000, the Danish air force until 1993, and the Austrian air force until 2005. The Draken also flew with the Flygvapnet ‘Acro Delta’ acrobatic team.

Design

The Draken is designed as a tailless middle double-delta wing fighter, with a single tail and a single engine (A Volvo Svenska Flygmotor RM6C, bestowing a maximum speed of 2125 km/h / 1,317 mph). Its double-delta wings allow good high and low speed performances. It also provided good fuel and armament capacity. The engine air inlets are located mid-wing at each side of the cockpit, featuring a characteristic egg shape.

Considered an easy-to-fly platform, yet not suitable for untrained pilots given the high sensibility controls, and being prone to ‘superstalls’ as a very stable platform with good low flight.

Although the avionics were in principle basic, the radar was a very sophisticated one – A PS-02/A based on the French radar Thompson-CSF Cyrano – integrated with an Ericsson version of a radar Thompson-CSF Cyrano S6 fire control system. It also incorporated VHF/UHF radio, a radio altimeter, a transponder, an IFF (Identification Friend or Foe) system, and the Swedish version of the Lear-14 autopilot. The seat of the pilot was reclined 30 degrees, similarly like the Viggen, to allow the pilot to resist G-forces. And the cockpit was fitted with air-conditioning and pressurization.

J35J Green Camouflage
J35J Green Camouflage

The engine in combination with the design, made the Draken a very manoeuvrable and fast fighter jet, with the braking parachute assisting the aircraft in the landing, reducing the distance required to reach a full stop. Earlier version of the Draken had two 30 mm Aden M/55 cannons, with later versions having only one cannon. Also some export versions kept the two cannons configuration.

An Advanced Cold Warrior

The Draken can boast not only being a radical and new design thus making it a very advanced one by the first decades of the Cold War. It was among the first fighters in incorporating an on-board radar and the earlier version of the data-link system, whose enhanced version was incorporated in the J 37 Viggen and the JAS 39 Gripen. Indeed, the Draken incorporated the STRIL 60 ground-control network that enable Draken pilots a firing guidance through the on-board instruments, being the system also capable to resist electronic jamming. Aside the fact of being the first European supersonic jet fighter, the Draken was the first fighter to have STOL capacities, and it was an aircraft that gathered valuable intelligence by producing photographic material of many new Soviet aircraft during the 70’s and 80’s. It also had a superior service ceiling in comparison with fighters of its times. Being a very resisting and long-endurance fighter, many pilots of the Draken stated that it was able to take on much newer designs.

Variants

  • J 35A – The first version of the Draken. Capable of performing fighter tasks. A small retractable wheel was placed on the rear fuselage as the angle of the nose was required to be elevated during landings to stop the airplane. But the wheel was also placed as the fuselage was enlarged, as the EBK 66 afterburner was incorporated. This version had 2 Aden 30mm cannons, installed on each engine air take, 2 to 4 Rb 24 (Swedish version of the AIM-9B Sidewinder missile) and a central fuel tank or an additional Rb 24. The afterburner installation allowed the Draken 35A to carry Bofors 135mm rockets (up to 12) in rocket pods. This version had basic avionics, being upgraded with the SB6 fire-control system, which included an infrared search and track sensor (IRST). 90 aircraft produced.
  • J 35B – Interceptor and fighter version. Its development began in 1956, before the J 65A was developed. It initially performed training task until better engines and avionics were available. This model then incorporated the air-to-ground STRIL 60 system, and new radar and fire-control systems that enhanced collision course interceptions. It had an ejection seat that allowed the pilot to eject at zero altitude. This version was armed with two 75mm Bofors cannons, folded-fin air-to-air unguided rockets, and for ground-attacks, 135mm rockets. 73 produced.
  • Sk 35C – Trainer version. Two-seat aircraft build upon J 37A airframes, being exported to Denmark and Finland. The second section was raised for the instructor’s place – being located right behind the pilot/student – and fitted with a 3D stereoscopic periscope. Upgraded with afterburners and improved avionics. The tail section was shortened, and the aircraft could be easily re-modified to its J 35A version if necessary. 25 delivered.
  • J 35D – Fighter version, equipped with a better engine – a Svenska Flygmotor RM6C – that made this version the fastest (up to Mach 2), which allowed increased payload, but also meant increasing fuel capacity. Its avionics were also upgraded, receiving a Saab FH-5 autopilot, an Ericsson PS-03 radar coupled with a Saab S7A fire-control system and a new ejection seat, replaced latter with a seat that allowed ejection on zero/zero conditions. 120 delivered.
  • S 35E – Reconnaissance version. It was unarmed but equipped with ECM measures. Fitted with seven cameras: a vertical-looking camera; a forward-looking camera on the nose; a downward/vertical looking with wide-angle camera and two sideways-looking cameras; and two long focal length vertical cameras. A downward-looking periscope and a voice recorder were fitted to allow the pilot to aim the cameras and make comments on the imagery. Latter improved with afterburners, chaff dispensers and two radar alerts, and the ability to carry on the central pylon a night-time Vinten Blue Baron multisensory night photography device. 60 delivered.
  • J 35F – Fighter version. It had improved avionics and electronics, such as integrated radars, radios, aim, infrared target seekers, and missile systems. In fact, it had the STRIL 60 incorporated. It was the version with enhanced armament, such as two semi-active radar homing Rb 27 AAM missiles, and two Rb 28 or Rb 24 AAM missiles. As a result of the new avionics, the second 30 mm cannon was supressed. Used by 18 squadrons in the Flygvapnet. 208 delivered.
  • J 35F2 – A J 35F fitted with a Hughes Aircraft Company N71 infrared sensor.
  • J 35J – Fighter version that kept the Draken in the inventories of the Flygvapnet, co-operating with the J 37 Viggen. It has six pylons, which increased the payload. It incorporated enhanced fire-control systems, infrared sensors, radar, altitude warning systems, navigation systems, IFF and modernised cockpit electronics. It also had a slightly improved RM6C engine that provided more speed. 76 delivered.
  • 35H – Proposed export version for Switzerland. None built or delivered
  • 35XD – Export versions for Denmark. It comprised the F-35 strike aircraft, TF-35 two-seat trainer and the RF-35 reconnaissance jets. Overall the 35XD were the heaviest aircraft of the Draken family, as they were optimized for strike missions. 51 delivered.
  • 35XS – Export version for Finland, some of which were locally assembled by Valmet under license in Finland. The received/assembled aircraft were the interception, fighter-bomber and training versions. 48 delivered.
  • 35BS – Used J 35B bought by Finland
  • 35FS – Used J 35F bought by Finland
  • 35CS – Used Sk 35C bought by Finland.
  • 35Ö – Version for Austria. Used J 35Ds that were refurbished and modernised by Saab, with extra 1000 flying hours, radar warning receivers, the radar of the J 35D, and chaff dispensers. Like the earlier version of the Draken, it was armed with the two 30 mm Aden cannons. 24 delivered.

Operators

  • Sweden – The Flygvapnet had 544 Draken: 90 J 35A; 73 J 35B; 25 Sk 35C; 120 J 35D; 60 S 35E; 208 J 35F; and 76 J 35J. Many were upgraded or modified airframes, so the number is an approximation. Many were sold to other countries.
  • Austria – The last exporter of the Drakens. The Österreicher Luftstreitskräfte received 24 J 35Ö – ex-Swedish J 35D – to replace the J 29F Tunnan in 1987. Initially many Draken (5 Sk 35C) remained in Sweden for training purposes, being replaced later by a simulator. The Austrian Draken were originally armed with two 30mm Aden cannons, as AIM missiles were restricted by a treaty after WWII. But as the crisis escalated in former Yugoslavia by 1993, deeming that cannons were not enough to protect the airspace, Austria acquired AIM 9P3 and AIM 9P5 Sidewinder missiles from the US and equipped them on the Draken.
  • Finland – The second exporter of Drakens, receiving 12 all-weather J 35XS interceptors, 7 ex-Swedish J 35BS, 24 ex-Swedish J 35FS and 5 ex-Swedish Sk 35CS, all to serve with the Suomen Ilmavoimat. Most of the received aircraft were delivered in kit form and assembled by Valmet in Finland, and had also two Aden 30 mm cannons. Finland used the Draken as interceptors and fighter-bombers, and retired them in 2000.
  • Denmark – The first country in exporting the Draken, with units being received in 1970. As the original version was the least favoured during the competition for a new Danish fighter, Saab created a new version (J 35XD), based on the J 35F. the structure was strengthened in order to allow more payload – 9 reinforced pylons – with simultaneous use possible. The landing gear was reinforced with an added arrestor hook, and had two Aden 30 mm cannons, as well as extra fuel capacity. Being a European cost-effective platform, plus the improvements, made the Kongelige Danske Flyvevåben to choose the Draken. 20 A 35XD ground attack fighters (denominated F35), 30 S 35XD reconnaissance (denominated RF35), and six Sk 35XD training (denominated TF35) were purchased. 7 additional aircraft were purchased to be cannibalized. Danish training and reconnaissance versions were fitted with cannons and pylons to carry weapons, thus having secondary combat capabilities. 5 further Drakens (TF35) were purchased. Receiving upgrades in the following years, the Draken were retired from Danish service in 1993.
  • US National Test Pilot School – Operated 6 Drakens, formerly Danish Air Force jets training and reconnaissance versions.

Draken Specifications
Wingspan 9.42 m / 30 ft 10 in
Length 15.20 m / 49 ft 10 in
Height 3.8 m / 12 ft 7 in
Wing Area 49.22 m² / 529.8 ft²
Engine 1 Svenska Flygmotor Turbofan RM6B
Maximum Take-Off Weight 10,089 Kg / 22,200 lb
Empty Weight 6.590 kg / 14,500 lb
Loaded Weight 16,000 kg / 35,273 lb
Maximum Speed 1,900 km/h / 1,200 mph
Range 3,250 Km / 2,020 miles
Maximum Service Ceiling 18,000 m /59,100 ft
Climb Rate 200 m/s ( 12,000 m/min / 40,000 ft/min )
Crew 1 (pilot)
Armament • 1 Aden 30mm Cannon
• 6 hardpoints that could allow 1700 kg of payload. A pod for a 135mm Bofors M70 rockets; air-to-air Rb 24, Rb 27 or Rb 28; external fuel tank; iron bombs; cameras.

 

Gallery

Saab J35J Draken - 35556 - Side Profile View
Saab J35J Draken – 35556
Saab 35Ö Draken - 351408 - Side Profile View
Saab 35Ö Draken – Austrian Air Force
Austrian Air Force Saab J35Oe Draken 351421
Saab J35Ö Draken – Austrian Air Force

Sources

Ängelholms Flygmuseum (n.d.). Flygplan J65 Draken Operational History., Boyne, W (December 2011). Airpower Classic. J35 Draken. Air Force Magazine, 94 (12), 68., Cpt. Moore, V. (2005). A Dragon’s Farewell. Warbirds, 28 (8), 12-16., Guerras del Siglo XX (1994). Guerras del Siglo XX, Aviones. Madrid, Spain: Editorial Altaya., Liander, P. (1999). Draken pensionerad. FlygvapenNytt, (1), 24-27., Martin, G. (2012). The Draken: One of Sweden’s finest fighters. Aircraft Information., Piccirillo, A. C. (2014). Elegance in Flight. Washington, DC: National Aeronautics and Space Administration., Sharpe, M (2001). Jets de Ataque y Defensa [Attack and Interceptor Jets, Macarena Rojo, trans.]. Madrid, Spain: Editorial LIBSA (Original work published in 2001)., WarbirdsUpdate (2013). The Swedish Air Force Historic Flight from Within the Cockpit. Warbirds News., Saab 35 Draken. (2016, April 2). In Wikipedia, The Free Encyclopedia., Winchester, J. (2012). Jet Fighters: Inside & Out. New York, NY: Rosen Publishing., X-Plane.org (2008). Dispersed Basing. X-Plane.org., Images: Draken in Flight by Alan Wilson / CC BY-SA 2.0, J35J Draken Exhibit by Alan Wilson / CC BY-SA 2.0