Tag Archives: Glider

Maeda Ku-6

 Empire of Japan (1943)
Experimental Glider Tank – One Mock-up Model

While tanks can provide excellent offensive firepower, they can’t always be easily transported to where they are needed. In the case of Japan during WW2, this was usually achieved by using ships and rail lines to transport them to where they were needed. Facing difficult terrain and disrupted shipping routes, the concept of a flying tank became a promising concept to the Japanese military hierarchy. By transporting tanks via the air, they could potentially offer benefits to the airborne troops, who were often left without proper heavy support. An exploration of this concept would lead to the creation of the Maeda Ku-6 tank glider.

The Concept of Airborne Operations

The American M22 Locust light airborne tank. (Source: Wikimedia)

The practice of dropping airborne troops behind enemy lines offers many tactical advantages, as they can attack weak points and enemy supply lines. This in turn would force the opposing side to redistribute its own forces away from the front to deal with this problem. On the other hand, airborne forces often lack proper artillery or armor support, making them vulnerable to well-equipped and directed enemies. Some nation armies responded to this by employing glider transportable light field artillery and even recoilless, high caliber guns. Transporting armored vehicles proved a more daring task to implement. Most tanks could not be easily carried inside a transport plane or even parachuted due to their weight and size. The American and British responded by developing lightly armored and armed tanks, such as the M22 Locust or the Light Tank Mk VII Tetrarch. The Soviet Union, on the other hand, designed an auxiliary glider contraption that would be used to transport a heavier tank, the Antonov A-40. This principle would also be tested by the Japanese Army during the war, which led to the creation of the Maeda Ku-6 project.

Antonov’s flying tank was unsuccessfully tested by the Soviets. (Source: Wikimedia)

Airborne Japan

The Japanese began the development of cargo glider designs for military use in 1937. Following the successful use of gliders by the Germans during their conquest of the West in May 1940, the Imperial Japanese Army began developing new gliders in June 1940. In response to this, the Imperial Japanese Navy began its own project soon after. In Japanese terminology, these were designated Kakku (English: to glide).

Both the IJA and IJN had and used parachute infantry units. It is important to note that these were relatively small units that were rarely employed in their intended role. For these reasons, their equipment was more or less the same as that of ordinary infantry formations. They saw the most active service during the fight for the Dutch East Indies in 1942. These were mainly used to capture various vital strategic points, such as airfields or weakly defended positions deep in the enemy’s rear line. Following the end of this campaign, the Japanese did not use paratrooper units in their primary role.

Japanese paratrooper IJN units had two notable deployments: in the successful Battle of Manado from 11th to the the12th January 1942, on Celebes Island, also known as Sulawesi, and in the Battle of Timor from19th February 1942-10th February 1943, where IJN paratroopers suffered heavy casualties. Their IJA counterparts were used more as a commando unit and were only ever airdropped during the invasion of Sumatra in February 1942.

Map of Japanese expansion by 1942. Some of these offensive operations also included the use of parachute units, albeit to a limited extent. (Source: https://www.pinterest.com/pin/389350330265435193/)

In 1943, attempts were made to increase their firepower, though, it is unclear how much impact the experiences from the airborne operations of February 1942 had. It was proposed to use specially designed glider tanks that could be flown to their designated target and thus provide necessary firepower to otherwise weakly armed paratrooper formations. In addition, this vehicle could be airlifted to any other theater of war without a need for them to be transported by ships, which were by this time, seriously endangered by the US Navy.

The Maeda Ku-6

The project was initiated by the Army Head Aviation Office in collaboration with the Fourth Army Research Center. The first drawings of this new design were soon ready and were allocated to the Maeda research center for the construction of a working prototype. In the early stage of development, the new tank was to be transported by a specially designed glider. But as Maeda was unable to create a glider that could transport a light tank, and so another solution was needed. Maeda engineers suggested another approach to this problem. As no glider could be developed to carry a tank, maybe the tank itself could be modified to use a glider.

While Maeda was responsible for the glider development, the design of the tank was given to Mitsubishi Heavy Industries. It is unclear if it was a completely new tank design or if Mitsubishi reused some of the existing vehicles that were in service. According to the Japanese Army and Navy Aircraft Complete Guide, the Type 98 light tank was used for the project. This tank was intended as a replacement for the Type 95 Ha-Go, but this was never achieved as it was built too late and in very small numbers.

The Type 98 light tank on which the Ku-6 was allegedly based. (Source: Wikimedia)

Name of the Project

According to E. M. Dyer, the new light tank was designated as So-Ra (Sora-Sha), which could be translated as the “sky” or “air” tank. The whole project would be designated Kuro-Sha, with the Ku and Ro, meaning the number ‘6’, taken from the Ku-6 glider designation. Lastly, the Sha stands for “tank”. An older source, J. E. Mrazek, mentions that the tank design originated in late 1939. According to Mrazek, the tank was initially designated ‘special Tank project 3’. It received the Sora-Sha designation before being changed to Kuro-Sha (English: Black Vehicle).

Technical Specification

The Ku-6 was designed as a tank transport glider. While not specified, it is likely that the Ku-6 would have been made out of wood. Due to the losses of the original documents, not much is known about its overall design. Over the years, historians based on available information devised two different designs of how this contraption may have looked.

The tank itself, due to its nature of use, had to be as light as possible. This means it would have been lightly armored and armed. The So-Ra’s total weight was slightly above 3 tonnes and would have been operated by two crew members. The driver was positioned in the front of the vehicle. He was also responsible for piloting the whole glider. Behind him, in the turret, was the commander, who was responsible for operating the main armament. This small crew would have greatly affected the tank’s overall performance. Given the limitation in size and weight, adding more crew members was not possible. In normal circumstances, the driver’s vision ports would have been small and protected. In this case, he would need to have a good and unobscured overall view of his surroundings. For this reason, he was to be provided with three large viewports. The armor was to be less than 12 mm thick. While its armament consisted of one 37 mm gun, along with a machine gun, a possible installation of a flame thrower was also considered.

The wooden mock-up of the Japanese airborne tank project. (Source: https://www.armedconflicts.com/Maeda-Ku-6-t41347)

As the tracks would cause massive drag during take-off, specially designed sleds would be attached to them to facilitate an easier take-off. According to the first proposals, the tank itself was designed to act as an improvised glider fuselage and the wings and the tail assembly would be attached to it.  The tank crews would be provided with wired controls installed inside the vehicle in order to pilot it. In front of the tank, a towing cable would be added to connect it to the glider tug.

In the first version, the wings were to be attached to the So-Ra sides with the tail assembly to the rear. (Source: https://www.armedconflicts.com/Maeda-Ku-6-t41347 https://imgur.com/a/xaLcNcO)

The second version is completely different. Above the tank, a larger wing with a twin tail boom was added. These two components would be connected by struts. In both cases, once the tank hit the ground, the wing assemblies could be easily removed, which meant that the tank could immediately go into action with relative ease.

The second version was completely different in appearance. (Source: https://www.armedconflicts.com/Maeda-Ku-6-t41347)

It is unspecified which material would be used during the whole wing assembly. Given its rather late introduction and Japanese limited resources at this point, wood would likely be used.  With the whole wing assembly, the Ku-6 had a length of between 12.8 to 15 m (depending on the source) with a width of 22 m and a height of 3 m. The wing area was around 60 m².

The maximum towing speed at heights of 4 km was 250 km/h. The maximum speed that could be achieved during the gliding flight itself was 174 km/h. The decent speed at 4 km altitude was 2.8 sec/m while at lower heights closer to the ground it was 2.6 sec/m. It is important to note that these are projected figures.

Testing and Project’s Fate

Due to the slow pace of work, the first operational glider prototype was completed in 1945. The tank itself was not ready by this time. As a temporary solution, a wooden mock-up of it with ballast was intended to be used instead. The prototype was taken to the sky by a Mitsubishi Ki-21 medium bomber. Almost from the start, the Ku-6 (according to E. M. Dyer the second variant was used) proved to have poor overall flight characteristics, and the pilot had a poor view. Lastly, as it was specially designed to carry the So-Ra, its transport capacity for other vehicles was very limited. The IJA officials quickly became disinterested in the Ku-6, focusing instead on the Ku-7 general purpose glider which looked more promising. Another aspect that we must take into account was the poor state of the Japanese Army in 1945. By this point, it was so battered and depleted, that undertaking an airborne operation was an impossible task. In the end, the Ku-6 would be terminated and the fate of the single prototype is unknown, but it was either scrapped or lost during Allied bombing raids.

The prototype was taken to the sky using a Mitsubishi Ki-21 aircraft. (Source: Wikimedia)
The Ku-7 was a more orthodox glider design. While they were built in small numbers, they would be mainly used for testing and were not used operationally by the Japanese Army. (Source: https://listverse.com/2015/09/29/10-goofy-warplanes-of-world-war-ii/)

Conclusion

The Ku-6 seems like an interesting concept that could have offered a number of benefits to the Japanese in the early years of the Pacific theater. By 1943, when the project was initiated, the war situation for Japan had rapidly deteriorated, with the Allies pressing on all sides. In reality, the Ku-6 proved to be too flawed in design. It was difficult to control and the pilot had poor visibility. Given that it was a glider, it would make an easy target for Allied fighters which, by its construction time, had almost complete air supremacy.

 

Specification Maeda Ku-6
Wingspan 22 m / 72 ft 1 in
Length 15 m / 42 ft
Height 3 m / 9 ft 8 in
Wing Area 60 m² / 645 ft²
Maximum Takeoff Weight 4.200 kg / 9.260 lbs
Maximum Gliding Speed 174 km/h / 108 mph
Maximum Towing Speed 250 km/h
Crew Two pilot/driver and the commander /gunner
Maeda Ku-6 hypothetical side wing configuration
Proposed version with the top wing construction.

 

Credits

  • Written by Marko P.
  • Edited by Henry H. & Medicman11.
  • Illustrated by Godzilla

Sources

  • D. Nešić (2008), Naoružanje Drugog Svetsko Rata-Japan, Beograd
  • E. M. Dyer (2009) Japanese Secret Projects Experimental Aircraft of the IJA and IJN 1939-1945, Midland
  • J. E. Mrazek (1977) Fighting Gliders of World War II, ST Martin Press
  • S. J. Zaloga (2007) Japanese tanks 1939-45, New Vanguard
  • Tomio Hara’s Japanese Tanks 1978
  • Japanese Army and Navy Aircraft Complete Guide
  • L. Ness (2015) Rikugun Guide To Japanese Ground Forces 1937-1945, Helion and Company

Ikarus 453MW

Yugoslavia flag Federal People’s Republic of Yugoslavia (1952)
Experimental Glider – 1 Prototype Built

The experimental Ikarus 453MW glider. [airwar.ru]
Following the end of the Second World War, the newly created Jugoslovenska Narodna Armija JNA (Yugoslav People’s Army) initiated a series of experimental aircraft design programs. These were intended for testing and gaining valuable experience in new jet propulsion technologies. From this initial work, an unusual new glider project, designated Ikarus 453MW, would emerge. Little is known about the purpose of this glider and its defined role.

The Unusual Glider

After the war, the once-proud Yugoslavian aviation industry was in ruin. Most of its firms had been either looted or destroyed, and many of the pre-war designers and engineers had been killed by the Germans during their retreat. The Allied bombing of Belgrade also inflicted further damage to the Yugoslavian industry’s infrastructure.  However, as the Yugoslav Partisans began liberating the country, some production facilities were slowly restored, as was the case with Ikarus in late 1944. The initial steps of the revitalization effort of the shattered Yugoslavia aviation industry were undertaken in late 1945 by the newly established Yugoslavian Air Force Command. A series of aircraft design teams were set up with the aim of creating a base for the new air force.

By the early 1950’s the overall situation changed to the extent that the Yugoslavian Army officials were ready to test various new technologies and designs. During this time, the Generalna Direkcija Vazduhoplovne Industrije GDVI (Directorate General of the Aviation Industry) led by Dragoljub Bešlin produced a series of experimental aircraft intended to test new design concepts. In 1952, work on an unusual inverted gull “M” shamed wing design began. The design team was also supported by the engineer Levačić. He was an experienced designer who worked with the British Royal Air Force during the war .

In the 1950s a series of experimental aircraft were produced including (from the left to the right side) Ikarus 452-2, 451M jet aircraft, and two prone-operated aircraft the Ikarus 451 and 232  acesflyinghigh.wordpress.com

The precise reasons for its commissioning and its history are not clear, but it appears that the Yugoslav army officials wanted to test a design that could offer a small and fast ground attack aircraft. When the design was ready, Ikarus was asked to construct the first glider prototype. If the glider design proved to have merit, the next step would be to equip this aircraft with a fully functional jet engine. It was designated the Ikarus 453MW, but it is also sometimes referred to as Р-453MW or GDVI-9. To avoid confusion this article will use the Ikarus 453MW designation. The MW  designation was used as the wings highly resemble these letters.

Technical Characteristics 

The Ikarus 453MW was a single-seat, mixed-construction experimental glider. Its fuselage was made of a metal base covered with metal sheets. The wings and tail assembly were made out of wood. The most noticeable characteristic of this glider was the use of unusual inverted gull m-shaped wings. The inverted gull wing design was used during the war by famous aircraft such as the German Ju 87 Stuka Japanese Aichi B7A and the American F4U Corsair. The Ikarus 453MW wings consisted of four parts. The part where the wings folded down was separated by two round-shaped gondolas. The wings were equipped with flaps and ailerons. The rear tail unit consisted of a simple rudder on the vertical stabilizer and did not have horizontal stabilizers.

The retractable landing gear consisted of four wheels. Two smaller wheels were located inside the fairly large wing gondolas. In the lower part of the fuselage, an additional and larger pair of landing wheels was located.

The cockpit was placed to the front of the central fuselage. The canopy was made of plexiglass but besides that, little is mentioned of the cockpit design.

While the experimental glider was unpowered, if successful it was planned to add two unspecified jet engines inside the wing gondolas.

 

The side and top drawing of the Ikarus 453MW. The wing design while unusual was not used on any other Yugoslavian aircraft design. Source: www.vazduhoplovnetradicijesrbije.rs
The Ikarus 453MW had a landing gear consisting of three landing wheels units. Two smaller ones are located in the wing gondolas and one in the central fuselage. Source: www.vazduhoplovnetradicijesrbije.rs

Testing and Cancellation of the Project

The Ikarus 453MW prototype was completed and ready for testing by November 1952. On the 28th of November, the first test flight was made by Metodije Bojković. The test flight was undertaken at the Batajnica Airfield near the capital of Belgrade. Unfortunately for all present, an accident occurred. During take-off, the glider veered off the runway. While the pilot was unharmed the glider was damaged and the test flight had to be temporarily postponed.

After repairs were made, additional aerodynamic wind testing was undertaken to test the overall design shape. As these proved satisfying, another test flight was to take place. The Ikarus 453MW was towed up to 3 km of altitude by an Ikarus 213 and then released. While the flight itself was without problems, another accident occurred during landing. After analysis of available data, it was concluded that the pilot was not to blame as he was not properly instructed on how to fly the Ikarus 453MW which had an unusual wing design. Following the second accident, an order was given by the Yugoslav Army officials to cancel the Ikarus 453MW project.

A Nuclear Carrier

Author  N. Đokić (Projektat Jugoslovenskog Strategijskog Bombardera) gives us an interesting reason for the Ikarus 453MW design. It is a generally lesser-known fact, but during this time, the JNA was highly interested in developing nuclear weapons. The JNA’s involvement in Yugoslavian nuclear research development is to this day still not completely clear. This source mentioned that according to some secret JNA documents, the Ikarus 453MW was intended to be an aircraft that could quickly deliver a nuclear warhead to enemy targets. For this reason, the final aircraft was to be able to carry one 2-ton nuclear warhead at a speed of 850 km/h. The operational range was to be some 2,000 km, and the maximum service ceiling was 11,000 meters. In the meantime, a contingent of F-84G jet aircraft was acquired from the United States. As these were capable of carrying nuclear weapons there was no need to further proceed with the Ikarus 453MW project.

Whether there is any truth to the nuclear weapons plans is difficult to determine. The JNA and the Yugoslavian political hierarchy were publicly known to be quite interested in developing nuclear capability. Of course, this would demand a massive amount of resources, highly trained personnel, and well-developed industrial capacity, all of which Yugoslavia simply lacked in these early years of its existence. Its industrial capacity and infrastructure were almost completely destroyed during the war, and it would likely, if at all possible, take decades of commitment and investment to actually build a nuclear weapon. Hypothetically, even if Yugoslavia was able to develop nuclear weapons in the following decades, all research and experience gained on the Ikarus 453 would be outdated by that time. In conclusion, it could not be ruled out that the JNA had overzealous and ambitious plans to test the concept of using a swift aircraft to deliver this weapon. In reality, Yugoslavia simply lacked any means to actually produce such weapons. Despite this, testing this unusual wing design, albeit in a limited manner, at least provided Yugoslav aircraft engineers with additional experience.

Surviving Model

While unfortunately the Ikarus 453MW glider was not preserved, a small model replica is on display at the Nikola Tesla Serbian Aviation Museum near Belgrade.

The Ikarus 453MW wooden replica is located in the Belgrade Aviation Museum. Source: www.vazduhoplovnetradicijesrbije.rs

Conclusion

The Ikarus 453MW was quite an interesting design mostly due to its unusual wing shape. Its overall history, especially the trials is somewhat obscure. While the prototype was involved in two accidents, this was not the fault of the design but rather poor communication with the pilot, who was not informed of its flight characteristics.

Specification Ikarus 453MW
Wingspan 7.5 m /  24 ft 7 in
Length 5.85 m / 19 ft 2  in
Height 2.01 m /  6 ft 7 in
Maximum Takeoff Weight 1,720 kg / 3,792lbs
Crew One pilot
Armament
  • None

 

Experimental Ikarus 453MW

Credits

  • Written by Marko P.
  • Edited by Henry H. & Ed J.
  • Illustrated by Carpaticus

Sources:

Blohm und Voss Bv 40

Nazi flag Nazi Germany (1943)
Glider-fighter – 6 prototypes

By the middle of the Second World War, the Germans were losing control of the skies over the occupied territories. Even the Allied air attacks on Germany itself were increasing. In an attempt to stop these raids, the Blohm und Voss company presented the Luftwaffe with a new project which involved using cheap gliders in the role of fighters. While a small series would be tested nothing came from this project.

The Bv 40 was designed as a cheap, armed, and armored fighter glider. This is the first prototype (PN + IA) which was lost on its second test flight. Source: https://www.flugrevue.de/klassiker/kampfgleiter-blohm-voss-bv-40/

History

By 1943, the German Luftwaffe (air force) was stretched to limits in an attempt to stop the ever-increasing number of Allied air attacks. The Allied Bombing campaign particularly targeted German war industry. During this time, there were a number of proposals on how to effectively respond to this ever-increasing threat. Proposals like the use of a large number of relatively inexpensive fighter aircraft, that were to be launched from larger aircraft, were considered with great interest. One proposal went even further by suggesting the use of an inexpensively modified glider for this role. This idea came from Dr. Ing Richard Vogt who was the chief designer at Blohm und Voss.

In mid-August 1943, Dr. Ing Richard Vogt handed over the plans of a cheap and easy to build (without the use of strategic materials which were in short supply) glider that could be built by a non-qualified workforce to the German Ministry of Aviation (Reichsluftfahrtministerium – RLM). The pilots intended to fly this glider were to be trained in basic flying skills only. The initial name of this Gleitjäger (glider fighter) was P186 which would later be changed to Bv 40. After receiving the initial plans the RLM responded at the end of October 1943 with a request for six prototypes to be built. The number of prototypes would be increased to 12 December 1943 and again to 20 in February 1944. If the project was successful, a production order of some 200 per month was planned.

One of the few built prototype is preparing for a test flight. Source: https://www.flugrevue.de/klassiker/kampfgleiter-blohm-voss-bv-40/

Design

The Bv 40 was designed as a partly armored and armed, mixed construction, fighter glider. Its 0.7 m (2ft 3 in) wide fuselage was mostly constructed using wooden materials, while the cockpit was provided with armored protection. The front armor of the cockpit was 20 mm (0.78 in) thick, the sides were 8 mm (0.31 in), and the bottom 5 mm (0.19 in) thick. Additionally, the cockpit received a 120 mm thick armored windshield.

The wings and the tail unit were also built mostly using wooden materials. The rear tail had a span of 1.75 m (5ft 9in). For towing operation, the Bv 40 was provided with a jettisonable trolley that was discarded once the Bv 40 was in the air. Once it was back to the airbase it was to land using a skid.

What is interesting is that in order to have as small a size as possible, the cockpit was designed so that the pilot had to be in a prone position. While a pilot prone positioned design offered advantages like being a smaller target and having an excellent view at the front, it also caused some issues like a bad rearview. While this design was tested in Germany (like the Akaflieg Berlin B9 for example), it was never implemented. Inside the cockpit, there were only basic instruments that were essential for the flight. In addition, due to the high altitude that it was supposed to operate, the pilot was to be provided with an oxygen supply system and a parachute. The side windows had sliding armored screens with integral visor slots that could offer extra protection.

Close up view of the small pilot cockpit. Source: https://www.flugrevue.de/klassiker/kampfgleiter-blohm-voss-bv-40/

The armament of this glider consisted of two 3 cm (1.18 in) MK 108 cannons. These were placed in the wing roots with one on each side. This was serious firepower which could cause a huge amount of damage to the target it hit. Due to its small size, the ammunition loadout was restricted to 35 rounds per cannon. The ammunition feed system was quite simple; it consisted of a rectangular ammunition feed hatch placed in the middle of each wing. Inside the wings, an ammunition conveyor chute was placed to guide the rounds directly to the cannons. There was also a secondary option which included the use of one cannon together with the ‘Gerät-Schlinge’ 30 kg (66 lb) towed guided bomb. This bomb was to be guided by the Bv 40 toward the enemy bombers and was then detonated at a safe distance. In practice, during testing, this proved to be almost impossible to achieve success.

The front view of the Bv 40. Note the towing cable and the release mechanism just behind it. The pilot was beside he armored cockpit also protected by a 120 mm thick armored windshield. The large box with the round capcel (marked as number 5) is the compass housing. Source: https://www.flugrevue.de/klassiker/kampfgleiter-blohm-voss-bv-40/

Other weapon systems were also proposed. For example the use of R4M rockets placed under the wings. There was also a proposal to use the Bv 40 in the anti-shipping role by arming it with four BT 700 type torpedoes or even using 250 kg (550 lbs) time-fused bombs. Due to the extreme weight increase, this was never possible to achieve.

How should it be used?

In essence, the glider was to be towed by a Me-109G to a height of around 6 km before being released. Once released, it was to engage incoming enemy bombers with its two 3 cm (1.18 in) cannons. If circumstances allowed, a second attack run was to be launched. After the attack, the pilot simply guided the glider to the nearby airbase. It was hoped that the small size and armored cockpit would be the pilot’s best defense.

Testing of the Prototypes

Once the first prototype (marked PN+UA) was completed in early 1944, the first test flight made at Hamburg-Finkenwerder was unsuccessful as it was not able to take-off from the ground. A second more successful attempt was made on the 6th (or 20th depending on the source) May 1944 at Wenzendorf. Despite being intended to have an armored cockpit, the first prototype was tested without it. It appears also that during the maiden flight it was towed by another unusual Blohm und Voss design: the asymmetrical Bv 141. But according to most sources, the Me-110 was to be used, which seems more plausible. After the first flight, some modifications to the jettisonable undercarriage were made. On the 2nd June 1944, the first prototype was lost during a crash landing.

The Bv 40 small size is evident here. Source: Pinterest

A few days later the second prototype (PN+UB) made its first test flight. During a dive, it managed to reach a speed of 600 km/h (370 mph). Its final fate is unknown but it was probably scrapped. The third prototype never took off from the ground as it was used for static structural tests. The fourth prototype (PN+DU) was lost during its first test flight but the precise date is unknown. The fifth prototype (PN+UE) made its first test flight on 6th July 1944, but its fate is also unknown. The last prototype (PN+UF) was tested with a new fin section and made its maiden flight on the 27th of July 1944.

During these test flights, the Bv 40 was able to achieve a flight speed of up to 650 km/h (404 mph). During dive testing, the following speeds at different altitudes were achieved: 850 km/h (528 mph) at 4,000 m (13,120 ft), 700 km/h (435 mph) and an astonishing 900 km/h (560 mph) at 5,000 (16,400 ft). Nevertheless, the results of the test flight appear to have been disappointing due to Bv 40’s poor overall flight performance.

The Bv 40 interior of the pilot cockpit. The Pilot was placed in a prone position. While this arrangement was tested on some German aircraft design in practice it was never implemented. Source: https://www.flugrevue.de/klassiker/kampfgleiter-blohm-voss-bv-40/

Rejection of the Project

Once the project was properly revised by the RLM officials, the obvious shortcomings of the Bv 40 became apparent. The Bv 40 was simply deemed too helpless against the Allied fighter cover. In addition, when the report of the first few prototypes was studied, it became clear even to the RLM that the Bv 40 was simply a flawed concept and so it decided to cancel it in mid-August 1944. The next month the Allies bombers destroyed the remaining 14 Bv 40 which were in various states of production.

Not wanting to let their project fail, the Dr. Ing Richard Vogt and the Blohm und Voss designers proposed to mount either two Argus As 014 pulsejets or two HWK 109-509B rocket engines under its wings. Nothing came from this as the Me-328 and Me-163 proved to be more promising (these ironically also ended in failure). There was even a proposal to modify the BV 40 to be used as a Rammjäger (ram fighter) which was never implemented.

Production

Despite initial requests for the production of 200 such gliders only a small prototype series would be built by Blohm und Voss during 1944.

  • Bv V1 – Lost during its second test flight.
  • Bv V2 – Fate unknown.
  • Bv V3 – Used for static testing.
  • Bv V4 – Lost during it’s first flight.
  • Bv V5 – Flight tested but final fate unknown.
  • Bv V6 – Tested with modified fin section.
  • Bv V7-V20 – Lost during one of many Allied bombing raids on Germany.

Operators

Germany – While testing was conducted on a small prototype series no production order was given.

The Bv 40 side view. Source: http://www.histaviation.com/Blohm_und_Voss_Bv_40.html

Conclusion

The Bv 40 on paper had a number of positive characteristics; it was easy to make, could be available in large numbers, was cheap, well-armed and it did not need skilled pilots. But in reality, the poor performance, lack of a power plant, low ammunition count, and its vulnerability to Allied escort fighters showed that this was a flawed concept. This was obvious even to RLM officials who put a stop to this project during 1944.

The Bv 40 drawings. The small rectangles in the middle of the wings are ammunition feed openings. Source: http://www.warbirdsresourcegroup.org/LRG/luftwaffe_blohm_und_voss_bv40.html

Gallery

Illustration by Ed Jackson

Blohm und Voss Bv 40

Blohm und Voss Bv 40 Specifications

Wingspan 25 ft 11 in / 7.9 m
Length 18 ft 8 in / 5.7 m
Height 5 ft 4 in / 1.63 m
Wing Area 93.64 ft² / 8.7 m²
Empty Weight 1.844 lbs / 830 kg
Launch Weight 2.097 lbs / 950 kg
Climb rate to 7 km In 12 minutes
Maximum diving speed 560 mph / 900 km/h
Cruising speed (when towed) 344 mph / 550 km/h
Maximum Service Ceiling 23,000 ft / 7,000 m
Crew
  • Pilot
Armament
  • Two 3 cm (1.18 in) MK 108 cannons
  • Or one 3 cm (1.18 in) MK 108 cannon and a glider bomb

Sources

  • J. Miranda and P. Mercado (2004) Secret Wonder Weapons of the Third Reich: German Missiles 1934-1945, Schiffer Publishing.
  • R. Ford (2000) Germany Secret Weapons in World War II, MBI Publishing Company.
  • Jean-Denis G.G. Lepage Aircraft Of The Luftwaffe 1935-1945, McFarland and Company.
  • M. Griehl (2012) X-Planes German Luftwaffe Prototypes 1930-1945, Frontline Book.
  • D. Herwig and H. Rode (2002) Luftwaffe Secret Projects, Ground Attack and Special Purpose Aircraft, Midland.
  • http://www.warbirdsresourcegroup.org/LRG/luftwaffe_blohm_und_voss_bv40.html
  • https://www.flugrevue.de/klassiker/kampfgleiter-blohm-voss-bv-40/