Английская Википедия:Arsenal VG 70

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The Arsenal VG 70 was a single-seat monoplane research aircraft flown in France shortly after World War II to assist in the development of high-speed jet fighters. Lacking an indigenous turbojet engine, the aircraft was fitted with a German Junkers Jumo 004. Unlike most jet-powered aircraft of the period, the swept wing was wooden as was the tail structure. The under-powered VG 70 made its maiden flight in 1948, but only flew five times before the program was terminated the following year.

Development and description

Jean Galtier, chief designer at Arsenal de l'Aéronautique, decided to build a turbojet-powered research aircraft in late 1945. He wished to investigate the aerodynamics of swept wings at high speeds to take advantage of captured German data to better understand how they might impact future fighter designs. Its all-metal fuselage was derived from the VG-30 prewar series of piston-engined fighters and Galtier took advantage of the company's experience of wooden construction to build the wing and empennage out of wood. The leading edge of the shoulder-mounted wing was swept back at an angle of 43° and the wing itself was given a dihedral of 6°. Seven fuel tanks were housed in the two-spar wing and dive brakes were positioned on its upper surface. The main wheels of the tricycle landing gear retracted into the wings while the nose gear retracted into the lower part of the nose.[1]

The Jumo 004 turbojet, captured from the Germans, had Шаблон:Convert of thrust. It was positioned in the aft fuselage, together with three additional fuel tanks, and used air provided by a prominent semi-circular ventral intake underneath the cockpit. Wind-tunnel testing showed that it was not as effective as had been hoped, although the airframe was deemed capable of reaching a speed of Шаблон:Cvt and Mach 0.9 in a shallow dive given enough thrust.[1]

Construction and flight testing

Construction of the aircraft was completed in 1947 and it had begun taxiing tests in October, but wind-tunnel testing revealed some potential aerodynamic problems that delayed its first flight by over six months. It finally flew on 23 June 1948 and achieved a speed of Шаблон:Cvt despite its unreliable engine. The program was cancelled in early 1949 after only five flights as the engine's lack of thrust imposed tight limits on the types of test flying that it could do and Arsenal had refocused on the follow-on VG 90 carrier-based fighter.[2]

Variants

Файл:02-ArsenalVG.70.01.png
Engineers and technicians surrounding prototype Arsenal VG.70.01

VG 70

Research aircraft powered by a Jumo 004 turbojet, one built[3]

VG 71

Research aircraft with a Rolls-Royce Derwent 5 turbojet, proposal only.[4]

VG 80

Carrier-based fighter aircraft powered by a Rolls-Royce Nene turbojet, never built, but developed into the VG 90.[4]

Specifications

Шаблон:Aircraft specs

See also

Шаблон:Portal Шаблон:Aircontent

References

Шаблон:Reflist

Bibliography

Шаблон:Commons category

Шаблон:Arsenal de l'Aéronautique

  1. 1,0 1,1 Buttler & Delezenne, p. 52; Carbonel, p. 35
  2. Buttler & Delezenne, pp. 52–54; Carbonel, p. 35
  3. Buttler & Delezenne, p. 52
  4. 4,0 4,1 Carbonnel, p. 36