North American P-500
During the period between both World Wars, the size and weight of the fighters was progressively augmented in parallel with the increasing power of the available engines. Against that general trend, there was a minority of aeronautical designers defending the small sized fighters, known as Jockey Fighters, at that time. This type of airplanes, if well designed, could generally compete in performance with the conventional fighters, using a less powerful engine, with an important save in fuel, manpower and strategic materials. They were also easier to maintain and store and their reduced size and weight helped to increase agility in combat, making more difficult to be seen by the rear gunners in the bombers, or by the pilots in the escort fighters, and their destruction required a higher consumption of ammunition.
At the beginning of World War II, the conventional fighters used to have 10 to 12 m of wingspan, operational weight of 2,500 to 3,500 kg and a maximum speed of 450 to 500 km/h. The light fighters of the time could be divided in two categories:
Jockey Fighters, with less than 10 m. wingspan, maximum weight of 1,800 to 2,500 kg and the same speed than the conventional fighters.
Midget Fighters, with less than 10 m wingspan, maximum weight of 600 to 1,800 kg and maximum speed of 350 to 400 km/h.
Since the mid-1930s, France was preparing for a long World War I-style attrition war against Germany.
Anticipating that the depletion of resources would affect the production of conventional fighters, l’Armée de l’Air issued several specifications calling for light fighters built in wood/plywood and engines with less than 800 hp. not to compete with the conventional fighters in the use of strategic materials.
On July 12, 1934, the Service Technique de l’Aéronautique laid down the Programme Technique de Chasseur Léger C.1, a specification for a lightweight interceptor with a maximum speed of 400 km/h and armed with four machine guns. The original specification was amended in August 22 dividing it in two categories: one for aircraft powered by 800-1,000 hp engines, armed with a cannon and two machine guns, to replace the outdated fighters Dewoitine D.500 and Loire 46, and another for 450-500 hp engines and two cannons. On December 17, 1934, the maximum speed rose to 450 km/h and on 16 November 1935 to 500 km/h. The winner of the first category was the Morane-Saulnier M.S.405, winning the production of the 860 hp Hispano-Suiza H.S.12 Y engines.
In the second category were competing small manufacturers and designers of racer airplanes experienced in obtaining the maximum speed with minimum power, often using self-made engines.
ANF Les Mureaux built the prototype 190, all-metal monoplane powered by an air-cooled inverted V-12 engine Salmson 12 Vars.
The project was abandoned due to design deficiencies in the power plant.
This engine may run at 4,000 rpm, with compression ratio 6, and a reduction box designed for firing an H.S. 404 cannon.
The success achieved by the Caudron racers, encourage designer Marcel Riffard to build the C.710 and C.713 prototypes, two wooden, cannon-armed, light fighters capable of flying to 455-470 km/h powered by a 450 hp air-cooled inverted V-12 engine Renault 12 R.01. On December 1937 l’Armée de l’Air dismissed its serial construction in favour of the Arsenal VG 30, much faster, with retractable undercarriage and better climb rate.
The wooden Arsenal VG. 30 was designed as a light fighter to fulfil the Chasseur Monoplace C.1 (June 3, 1937) specification that called for a small fighter propelled by one 690 hp Hispano-Suiza H.S.12 X crs engine and armed with one 20-mm H.S.9 cannon and two 7.5 mm MAC 34A drum-feed machine guns, from the obsolete Dewoitine D.510 fighters.
Fifteen days after the declaration of war on Germany the S.N.C.A. du Nord received a commission for the manufacture of 220 units of the VG 33, later expanded to 500. Deliveries to l’Armée de l’Air should start at the beginning of 1940. But there were problems with the import of spruce from Canada and Romania and only seven planes entered combat between 18 and 25 June 1940.
The Potez firm proposed the model 23, a high-performance small all-metal airplane fitted with retractable undercarriage that could use some technical elements left aside by first line fighters.
Thus, the surplus of Hispano-Suiza H.S.12 Xcrs engines, H.S.9 cannons and MAC 34A machine guns coming from the obsolete Dewoitine D.510 fighters could go back to combat without overloading the French war production of H.S.12 Y-45, H.S.404 and MAC 34 M39, intended for the Dewoitine D.520. Would the new equipment be available in enough quantity, it would also have been used by the Potez 230 as it was compatible to both.
A prototype was built in the Potez C.A.M.S. factory of Sartrouville in 1939. During a series of tests performed in the Villacoublay test centre in March 1940, it reached the speed of 560 km/h being equipped with an H.S.12 Xcrs of just 680 hp (the Dewoitine D.520 reached 525 km/h and the Bf 109 E-1, 575 km/h with much more powerful engines).
On January 12, 1937, l’Armée de l’Air issued the specification Programme technique A.23 calling for a light fighter able to fly at 520 km/h powered by one air-cooled radial engine Gnôme-Rhône 14 M rated at 690 hp.
The Roussel R.30 was conceived as a private venture all metal Jockey Fighter. Construction of the prototype began at Courbevoie, flying for the first time in April 1939.
In August 1939 it was transferred to the Centre d’Essais du Matériel Aérien (C.E.M.A.) for official trials, because of which it was recommended to install a more powerful engine to better use its excellent flying performances. During the Battle of France, the airplane was armed with two 20-mm Oerlikon FFS cannons mounted in the wings and some tests were performed for the installation of a bomb rack under the fuselage.
The Bloch M.B.700 was also designed as an answer to the Programme technique A.23. This small interceptor differentiated from the Roussel in that it was built from wood. Outwardly, it looked like an 83% scaled down version of the conventional fighter Bloch M.B.152. The main advantage of the M.B.700 reduced size was that while equipped with an engine with 75% the power of an M.B.152, it flew 80 km/h faster, still carrying the same armament, and was a more difficult target in dogfight.
In 1939 a prototype was built in the Blériot-Aéronautique of Suresnes, flying for the first time by mid-April 1940.
After the Third Reich annexation of Sudetenland, the Polish Department of Aeronautics issued the Sokół specification, calling for a light-weight single seat fighter powered by one 660-730 hp Gnôme-Rhône 14M-05 Mars double-row radial engine.
The P.Z.L. firm proposed two Sokół versions, with all-metal construction, semi-monocoque fuselage structure and P.Z.L. two-blade, adjustable pitch airscrew: the P.45/I with fixed undercarriage and the P.45/II with retractable undercarriage. The estimated maximum speed of the P.45/II was 520 km/h.
The Design nº 25 proposed by the firm R.W.D. was very similar to the Fokker D.XXI and used the same construction system.
This version of the Sokół, would have an estimated maximum speed of 450 km/h.
The Design nº 42, proposed by the firm P.W.S. would be totally built of wood/plywood, with inwards retractable landing gear.
Its estimated maximum speed would be 520 km/h.
In anticipation of political circumstances prevented the import of the Italian fighters, the Danish Naval Shipyard Orlogs Vaerftet began working on the design of the OV-J-1 Marinejager. It was a single-seat light fighter powered by an inverted-Vee, air-cooled engine, of the type of Walter Sagitta or Isotta Fraschini Delta. It would have been completely manufactured in metal, with retractable landing gear.
In 1939, the Latvian local industry Valsts Elektro-Fabrika (VEF) produced
the VEF I-16 wooden light fighter powered by one 520 hp. air cooled, inverted V-12 engine Walter Sagitta ISR with a maximum speed of 460 km/h.
By the time of the Munich Crisis, it was unclear to the British authorities if the production of the new monoplane Hawker Hurricane and Supermarine Spitfire fighters could be accelerated sufficiently to equip the 123 Squadrons that the Fighter Command required for the defence of the British Islands.
In October 1938, F.G. Miles, designer of the Miles Master advanced trainer, proposed the construction of a single-seat fighter that could supplement the Hurricanes and Spitfires already in production, without competing with them for the Merlin engines or in the use of strategic materials. The project, called Miles M.20/1 Munich Fighter, could be built entirely of wood/plywood using the retractable landing gear and several parts of the Miles Master trainer.
It would be propelled by one 885 hp liquid-cooled V-12 Rolls-Royce Peregrine engine, driving a two-bladed airscrew and would be armed with two 20-mm Hispano-Suiza H.S. 404 cannons. A wooden mock-up was built at the end of 1938, but no orders were placed because production of the Peregrine was reserved for the Westland Whirlwind twin engine fighter.
Miles persisted with the M.20/2 project, adapted to the Specification F.19/40, calling for a fighter armed with eight 0.303-in Browning Mk. II machine guns and propelled by one 1,300 hp Rolls-Royce Merlin XX 'power egg' interchangeable with the Bristol Beaufighter and the Avro Lancaster airplanes. The M.20/2 had a fixed landing gear, thus removing the need of hydraulic circuits and enabling the construction in fourth the time than a Hurricane and tenth time than a Spitfire. During the flying tests carried out on September 14, 1940, the prototype AX 834 showed a top speed exceeding that of the Hawker Hurricane Mk. I and manoeuvrability equivalent to that of the Supermarine Spitfire Mk. I. The stabilization of the German offensive and the increase in production of the conventional fighters rendered it mass production worthless and the project was left aside in April 1941.
The projected fighter Percival P.33 AB, based on the aerodynamic configuration of the Mew Gull racer that competed for the Merlin XX engine, was also cancelled. It would have been a 556 km/h fighter.
During the critical days of 1940 the Panic Effect boosted numerous interim solutions to increase the number of fighters available: A.A. Bage, the Percival chief designer, proposed to build a version of the Mew Gull armed with two 0.303 in Vickers Mk. II machine guns. The projected light fighter, called Percival P.32 AA, was rejected in favour of the Miles M.24, the single-seat version of the Miles Master, capable of flying at 370 km/h and with handling characteristics like those of the Hawker Hurricane.
The Panic Effect caused by the Munich Agreement forced the French Government to carry out large, massive purchases of foreign aircraft, but it turned out that the production capacity of Curtiss and Boeing was saturated by the enormous orders of planes made by British.
The panic increased. Left to their own devices, the weak countries had three options only: to improve the fighters at their disposal, to develop new fighters from advanced trainer planes or to build them from scratch creating their own panic fighters. Swedish and Finnish tried the latest solution with average results, due their lack of experience. The old Swiss and Finnish Morane 406 were equipped with more powerful engines in a try to expand their operational life. Australians, Peruvians and Thais bought fighters based on the North American Texan trainer. British, Lithuanian and Latvian modified their Miles Master, Irbitis and Aviotehase trainers to use them as emergency fighters.
The U.S. military showed no interest in lightweight fighter until the early months of World War Two but North American Aviation Inc. (NAA) was a new company in the aviation industry interested in capturing new business.
In 1938, the General Manager James H. Kindelberger and a representative from Export Sales traveled to England to formalize the export contract for 200 AT-6C/D Harvard trainers.
When it became clear that the development of the Napier Sabre engine would not be completed in time to power the new Hawker Thyphoon and Martin-Baker M.B. 3 fighters that were to replace the Hurricane and Spitfire, British suggested to Kindelberger that NAA build a new fighter of its own.
But the project was frozen for two years because of laws regulating the export of U.S. technology.
After the cancellation of the NA-53 fighter on February 3, 1939, because its engine was too powerful, NAA decided to enter the European market for light fighters powered by air-cooled, inverted V-12 engines.
A new design program called SC-46 (Shop Charge) was issued on December 18, 1939.
A team consisting of designer Edgard Schmued and drawer Al Algier began working on the concept P-500, a light fighter that was ready for presentation to British Air Ministry and Armée de l’Air representatives on January 23, 1940.
The new fighter was powered by one Ranger SGV-770C-1C rated at 520 hp., but the British Purchasing Commission were only interested in acquiring many conventional fighters and suggested to NAA the manufacture of Curtiss Hawk 87 A-1 (P-40D) fighters and rejected the P-500 concept.
On February 6, NAA offered the French a cannon-armed variant powered by one Fairchild-Ranger XV-770-9 engine fitted with two-speed Szydlowski-Planiol mechanical supercharger and superimposed gear box but the Service Technique de l’Aéronautique had already decided to use two hundred units of the Caudron C.R. 714 that had just entered service in January with Armée de l’Air as an advanced trainer.
On April 25, 1940, the U.S. Government restrictions of exportation were lifted, and NAA was able to concentrate on the design of the NA-73 (the future Mustang) in competition with the Curtiss XP-46.