Ā Italy (1940)
Fighter Bomber – 48 Built
Following the failure of the Re.2000, the engineers from Reggiane tried to design a new aircraft to fill the role of ground attack aircraft. This would lead to the development of the improved Re.2002 aircraft. While the Regia Aeronautica (Italian Air Force) ordered 500 of this version, due to problems with production, only about half of that number were ever built.
History
In the late 1930s, Italian aircraft manufacturer Reggiane was attempting to gain attention from the Reggia Aeronautica with its Re.2000. While this aircraft initially showed good flying performance, it was not adopted for service. For this reason, Reggianeās chief engineer, Roberto Longhi, set out to develop a new aircraft that would fulfill the role of a fighter-bomber aircraft, which the Italian Air Force was in desperate need of. Roberto Longhi made sure to address the shortcomings of the Re.2000ās fuel tanks when designing the new aircraft. These were prone to leaks, so he replaced them with conventional fuel tanks. For this new aircraft, that would later be known as the Re.2002 Ariete (Ram), a large 1,175 hp Piaggio P.XIX R.C.45 Turbine (Whirlwind) – D 14 cylinder air-cooled radial engine was chosen. The Piaggio P.XIX R. engine was still in the development phase at that time and not yet ready for service. The choice of using an engine still in the development phase would have a great negative impact on the later production of the aircraft. A radial engine was preferred over an inline liquid-cooled engine due to the fact that it was durable and less vulnerable to ground anti-aircraft fire. The new aircraft had a number of similarities to Reggianeās earlier designs, possessing the overall shape of the Re.2000, and the Re.2001ās internal construction.
First Test Flight
The maiden flight of the Re.2002 (M.M. or MM 454) prototype took place in October 1940. It was flown by test pilot Mario de Bernardi. After the first flight, the pilot noted that the Re.2002 had good general flying performance, but there were problems with the engine overheating. After several more test flights, constant engine overheating problems forced further flights to be halted, and the aircraft was returned to Reggiane for necessary engine modifications. After a number of upgrades to the engine were completed in March 1941, the test flights continued. During these tests, the Re.2002 managed to achieve a top speed of 417 km/h (260 mph).
Technical Characteristics
The Re.2000 was designed as a low wing, all-metal construction single-seat ground attack plane. The fuselage consisted of a metal frame covered with aluminum sheets held in place by using flush-riveting. The elliptical wings were built using a metal frame covered with a stressed skin duralumin structure. One fuel tank was located in each wing, with an additional third one placed just behind the pilot. If needed, additional auxiliary fuel tanks could be added under the fuselage or the wings.
The landing gear system was unusual, but standard for Reggiane aircraft. When it retracted backward, the wheel rotated 90Ā° before it retracted into the wheel bay. For better landing, the landing gear was provided with hydraulic shock absorbers and pneumatic brakes. The smaller rear wheel was initially retractable, but was changed to a fixed type at the start of production. The Re.2002 was powered by a 1,175 hp Piaggio P.XIX R.C.45 Turbine-D 14 cylinder air-cooled radial engine derived from the french Gnome-RhĆ“ne 14K Mistral Major. This engine was equipped with a three-blade variable pitch Piaggio P. 1001 propeller made by Piaggio.
The initial cockpit canopy was unchanged from the Re.2000 and opened to the rear. The production version had a canopy taken from the Re.2001. This canopy opened to the side.
The Re.2002 possessed the same offensive capabilities as its Re.2001 cousin. It consisted of two Breda-SAFAT 12.7 mm heavy machine guns mounted in the engine cowling. The ammunition load for the left machine gun was 390 rounds, with 450 rounds for the right. Two additional 7.7 mm Breda-SAFAT machine guns were placed in each wing. The ammunition load for the right machine gun was 350 rounds and 290 rounds for the left.
Being designed to act as a ground attack plane, the Re.2002 was equipped with one bomb rack placed under the fuselage with an additional rack placed under each wing. The central bomb rack could carry up to 650 kg (1,430 lb). The smaller wing racks could each carry up to 160 kg (350 lb) of payload.
Production for the Italian Air Force
Following the completion of test flights, the Italian Air Ministry (Ministerio dellāAeronautica)Ā gave an order for 200 Re.2002s to be produced. The first production aircraft were completed in October 1941. Due to engine production difficulties, the distribution of new aircraft to front line units was only possible in late 1942. While the initial order of 200 was increased to 300, only between 48 to 147 (depending on the source) were built for the Italian Air Force by September 1943. Initially a production order of 200 was placed in March 1942, which would be increased to 300 later in 1943. The sources unfortunately disagree about the number of produced aircraft. For example, sources like J. F. Bridlay (Caproni Reggiane Re 2001 Falco II, Re 2002 Ariete and Re 2005 Sagittario) listed a production number of 147 aircraft, which is the highest number listed in the sources. Other like DuÅ”ko NeÅ”iÄ (Naoružanje Drugog Svetsko Rata-Italija) and David Monday, (The Hamlyn Concise Guide To Axis Aircraft OF World War II) gives us a number of 50 aircraft. While George Punka (Reggiane Fighters In Action) gives us a number of 48 aircraft. All previous numbers do not include later aircraft, especially built for the Germans which is often listed as around 60 or so.Ā The lower production numbers were due to many reasons, lack of production capabilities, scarce resources, supply problems with engines, among others. The disagreement among sources may be the consequence of confusing the number of produced versus actually delivered aircraft.
Further Development
With only a small number of aircraft ever built, there were only a few known modifications and proposals for the Re.2002. One was an experimental version created by combining the Re.2002ās fuselage with the Re.2005ās wings. This aircraft was known as Re.2002 bis, but was never truly completed. The second version was to be used on two Italian aircraft carriers, the Aquila and Sparviero. While catapult launch tests were conducted on at least one Re.2002, due to the cancellation of the Italian aircraft carriers, construction of this version was never pursued. One Re.2002 was tested in the Re.2003 two-seater reconnaissance aircraft configuration. As the Re.2003 was not adopted for service, only one prototype was built. The last proposal included a torpedo carrier version, but this was never implemented. The majority of these do not appear to have received any special designation.
In Italian Service
After the introduction of the Re.2002 into service, some additional changes were made in comparison to the prototype. These include: improvements to the engine cowling, introducing a fixed rear tail wheel, and changing the canopy with a new one based on the Re.2001. The improved engine cowling actually caused some issues during dive-bombing runs, as the engine would sometimes simply stall. From the 17th aircraft onward, a new lower engine mount was tested with a different cowling type.
Delivery of the first operational Re.2002 for militaryĀ use was only possible in November 1942. The Re.2002s were allocated to the 102Āŗ Gruppo, with its 209ĀŖ and 239ĀŖ Squadriglia, stationed at Lonate Pozzolo. This unit had experience operating ground attack aircraft, previously operating German-supplied Ju-87 dive bombers. The next month, the 101Āŗ Gruppo, with its 208ĀŖ and 238ĀŖ Squadriglia, also began to receive their first Re.2002s to replace their outdated FIAT C.R. 42 biplanes.
During the Allied invasion of Sicily in July of 1943, the Italian Air Force stationed there had only 165 operational aircraft. Two groups, equipped with some 32 Re.2002 in total, were also present as part of the 5Āŗ Stormo. The first combat action was on the day of the invasion on the 10th of July, when Re.2002s managed to sink an Allied transport vessel called Talamba. Four aircraft and the commander of the 5Āŗ Stormo Colonel Guido Nobili were lost during this action. The next day, a group of 11 Re.2002s began a new attack on the Allied ships stationed near Augusta-Syracuse. The British battleship HMS Nelson was damaged with a 250 kg (551 lbs) bomb, with the mission resulting in the loss of two Re.2002s. In retaliation, the Allies bombed the Re.2002 airfields a few hours later. Due to losses, the surviving Re.2002s were repositioned to Manduria. After receiving reinforcements, the Re.2002s attempted another attack on July 19th, but lost six aircraft in the process. On 20th and 26th July, transport ships Pelly and Fishpool were sunk.
In early September 1943, Allied forces landed in Southern Italy. The Italian command, in despair, dispatched a small group of aircraft supported by 15 Re.2002s in an attempt to drive them back. On 8th September, 1943, due to immense Allied pressure and rising military losses, the Italians surrendered. By this time, the 101Āŗ and 102Āŗ groups had only 24 Re.2002s, but only half were combat ready. During the two months of fighting, some 32 aircraft were lost. While 19 were lost in direct combat, the remaining were destroyed in Allied bombing actions or accidents.
In early September 1943, the 50Āŗ Stormo, with its 158Āŗ and 159Āŗ Groups, was undergoing the process of conversion to the Re.2002. But, due to Italian capitulation, only the 159Āŗ Group received Re.2002s which were not used operationally.
In German Hands
Following the Italian capitulation, Germany launched Operation Achse (Axis) with the aim of capturing a large portion of the territory of their former ally. This included a number of production facilities, such as the Reggiane factories. The Germans seized some 14 fully completed aircraft, and around 10 more which were under construction. As there was sufficient material available, the production of the Re.2002 continued for some time under German supervision. Due to the same persistent engine delivery problems, Reggiane officials proposed mounting the 1,600 hp BMW 801 engine in the Re.2002, along with other modifications such as an updated wing design. One engine mount was tested in Germany, which led to a production order of some 500 new aircraft in late 1943. However, as the Reggiane factories were destroyed in early 1944 by an Allied bombing raid, the delivery of this modified version was impossible. In the meantime, some 60 aircraft were produced by Caproni under German supervision. Reggiane was actually owned by Caproni, thus all the necessary tooling and equipment for the continued production of this aircraft was available. Not all 60 were accepted for service by the Germans. Due to the Allied advance in April 1945, around 25 were seized by the Germans, while the remaining airframes were destroyed. Additionally, two aircraft were built at Biella. Unfortunately, the exact use of these aircraft by the Germans is not well documented. For example, it is unknown if they were ever used against the Allies in Italy. It is known that these were used by Geschwader Bongart against French resistance around Limoges, Vercors, and Aisne in 1943 and 1944.
On the Allied Side
Smaller groups of around 40 Re.2002s, that were previously used by 5Āŗ Stormo, were operated by the new Aeronautica Cobelligerante Italiana (Italian Co-belligerent Air Force) in cooperation withĀ the Allies. In October 1943, these were used to form the Gruppo Tuffatori, a dive-bombing group. In 1943, they saw action in supporting the Italian Resistance Movement in Northern Italy, an area which was controlled by the Germans. In 1944, they were also employed in attack operations across the Adriatic Sea, towards the Yugoslavian coastline. One of the last combat missions of the Re.2002 was a bombing run against Axis targets in Dubrovnik on 29th March, 1944. While the Co-belligerent Army lost 9 aircraft in combat, further combat missions had to be aborted due to a general lack of spare parts, their operational life lasted less than 12 months. The surviving aircraft were reallocated to the Fighter Training School at Lecce-Leverano in June 1944. There, they were used for pilot training for a few months, before they had to be discarded, once again due to a lack of parts and poor mechanical condition.Ā
Production Versions
- Re.2002 (MM 454) – Prototype aircraft
- Re. 2002 – Production version
Prototypes and Proposed Versions
- Re. 2002 bis – An experimental version created by combining the Re.2002ās fuselage with the Re.2005ās wings. One built, but never used operationally.
- Re. 2002 Aircraft Carrier Version – possibly one modified for this role
- Re. 2002 – Proposed torpedo carrier version
- Re. 2002 – Powered by a 1,600 hp BMW 801 engine. While the engine mount was tested and a production order was given, no aircraft were ever fully completed
- Re.2002 – One aircraft modified and tested as Re.2003
Operators
- Kingdom of Italy –Ā 147 aircrafts were delivered to Regia Aeronautica
- Germany – After the Italian surrender to the Allies, Germany seized around 60 aircraft.
- Esercito Cobelligerante Italiano – Operated some 40 Re.2002 aircraft
Surviving Aircraft
Today, there are only two surviving Re.2002 aircraft. One was located at the Italian Air Force Museum. The second incomplete Re.2002 can be seen at the French MusƩe de la RƩsistance et de la DƩportation of Limoges.
Conclusion
While the Re.2002 proved to be able to fulfill the role of fighter-bomber that the Italians were lacking. Due to a number of factors, its production was severely hindered. While work on the Re.2002 began in 1940, the production could not start before late 1942. Due to engine delivery problems, only a small number of aircraft were ever delivered to the Italian Force. Its first action against the Allies in Sicily ironically proved to be their last under the Fascist regime. While some would be used up to the warās end, due to a lack of spare parts, most would be used as training aircraft until finally being discarded.
Re.2002 Specifications |
|
Wingspans | 36 ft 1 in / 11 m |
Length | 26 ft 9 in / 8.16 m |
Height | 10 ft 4 in / 3.15 m |
Wing Area | 220 ftĀ² / 20.4 mĀ² |
Engine | One 1,175 hp Piaggio P.XIX R.C.45 Turbine (Whirlwind)-D 14 cylinder air cooled radial engine |
Empty Weight | 5,270 lbs / 2,390 kg |
Maximum Takeoff Weight | 7,140 lbs / 3,240 kg |
Climb Rate to 6 km | In 8 minute 48 seconds |
Maximum Speed | 267 mph / 430 km/h |
Cruising speed | 250 mph / 400km/h |
Range | 683 miles / 1,100 km |
Maximum Service Ceiling | 36,090 ft / 11,000 m |
Crew | 1 pilot |
Armament |
|
Gallery
Illustrations by Carpaticus
Credits
- Written by Marko P.
- Edited by Stan Lucian & Ed Jackson
- Illustrations by Carpaticus
- DuŔko N. (2008) Naoružanje Drugog Svetsko Rata-Italija. Beograd.
- M. Di Terlizzi (2002) Reggiane RE 2000 Falco, Heja, J.20, Instituto Bibliografico Napoleone.
- G. Cattaneo (1966) The Reggiane Re.2000, Profile Publication Ltd.
- J. W. Thompson (1963) Italian Civil And Military Aircraft 1930-1945, Aero Publisher
- G. Punka (2001) Reggiane Fighters In Action. Signal Publication.
- Re.2002 Photographic Reference Manual
- C. Shores (1979) Regia Aeronautica Vol. I, Signal publication.
- J. F. Bridlay (1972) Caproni Reggiane Re 2001 Falco II, Re 2002 Ariete and Re 2005 Sagittario, Profile Publications
- David. M, (2006) The Hamlyn Concise Guide To Axis Aircraft OF World War II, Bounty Books.
- Images: Rod’s Warbirds Reggiane Re-2002 Ariete II – Ā http://www.vvsregiaavions.com/RegiaHTML/rre20021.htm