The priority of the German aircraft industry in jet aircraft does not diminish the role of other countries that have joined before the Second world war in the “reactive” race. And each of them has contributed to this difficult process. Am Cradle started to design the turbojet engine (TRD) in the mid-thirties of the last century and do not start a war, probably would have completed it before.
In the UK, a retired military pilot Frank whittle, who founded in 1936 the company “Power jets” for three years worked on the creation of the first turbojet engine. By mid-1939, they built W. 1 centrifugal compressor “issued” on the stand rod 270 kgs.
Works Whittle became interested in the British Air Ministry, who offered the firm “Gloucester” build experimental aircraft with turbojet according to specification E. 28/39. “Pioneer” was the title of this car really became the firstborn jet aircraft in the UK, once a global aviation power.
The official contract for the construction of the machine was issued to the firm in February 1940 Developed by John Carter single-engine aircraft built over a year in duplicate. And this despite the novelty of the design and many technical problems! On 7 April 1941 the first car with factory code W4041/G appeared at the airfield of the company, “Gloucester” Hucclecote. The letter “G” in the code meant that this “miracle of technology” was supposed to be under constant armed guard.
After delivery of the apparatus to the airfield chief pilot of the company Harry Sayer began taxiing and Jogging, but may 15 was the first flight, which lasted 17 minutes.
Flying “Pioneer” fully confirmed the promise of the idea of creation of reactive machines, despite the low thrust of the engine and its reliability. Both the experimental sample until 1944 served as a flying laboratory, which worked out new, more advanced engines. In April 1946 the plane was transferred to the British Museum of science and technology where he is today.
“Pioneer” opened the way for the application of turbojet engines for airplanes, but unfortunately, because of the small thrust motors W. 1 W. 1A and nothing, except yourself, in the air could not raise. Therefore, British manufacturers have concentrated on designing more powerful engines, and the airplane people, led by Carter — on a heavy twin-engine fighter specification G. 9/40. Work in this direction was carried out from August 1940
The task of designing a combat vehicle Carter got in November. The war Department issued an order for the building immediately. 12 prototypes. However, later it was reduced to six cars, but then increased to eight.
In December, the engineering team has completed the overall layout of the aircraft, designated G. 41. He was a single-seat monoplane with the nose landing gear and stabilizer placed on the middle of the keel. Both engines have a “wing”. Of all the examined layouts, this location provided the best approaches to the motors during their operation and repair, which was considered important due to the low reliability of the first turbojet engines.
The armament of the new fighter according to customer’s requirement was to consist of six 20-mm guns with ammunition 120 rounds. During the design it became clear that the location of a couple of guns under the cockpit are extremely uncomfortable and unsafe. Carter managed to convince the Ministry of aviation that it is reasonable to reduce the number of guns to four. However, ammunition for the remaining guns was increased to 150 rounds.
Looked very promising scheme of the technological division of the glider on several large sites that could be collected in parallel at different plants. The bow section is included the pressurized cabin of the pilot (created in cooperation with the firm “Westland”); weapons bays and the nose landing gear. However, the pressurized cabin to the “meteor” appeared later, in the modification of F. 8.
The middle part of the fuselage, which housed the fuel tank and cartridge boxes, combined with the center section and the nacelles of the engines. The latter is attached only to the front side member and the flange of the rear spar made a cutout for installation of the jet nozzle. In the center was placed the main landing gear.
The third major section was the tail section with the tail.