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VFW VAK 191B

From Wikipedia, the free encyclopedia

VAK 191B
VAK 191B next to Do 31 transport
Type VTOL strike fighter
Manufacturer Vereinigte Flugtechnische Werke
Maiden flight 20 September 1971
Status Retired
Primary user Luftwaffe
Number built 3

The VAK 191B was an experimental German VTOL nuclear strike fighter.

It was produced by a German consortium known as 'VFW' (Vereinigte Flugtechnische Werke) consisting of Focke-Wulf, Heinkel and Weser. Initially Fiat of Italy was also involved but dropped out in 1967, though remaining as a major sub-contractor. VAK means Vertikalstartendes Aufklärungs und Kampfflugzeug (V/STOL Reconnaissance and Strike Aircraft.)

Propulsion was provided by a Rolls-Royce/MTU RB.193-12 vectored thrust engine for both lift and cruise which was augmented by two vertical lift engines.

The program was begun in 1962 to replace the Fiat G.91 ground attack fighter with a VTOL aircraft but NATO requirements changed and it became a technology demonstrator. Three VAK 191B aircraft were flown in the flight test program between 1970-1975 making 91 flights. The first hovering flight was made in Bremen on 20 September 1971. The first transition from vertical flight to horizontal and vice versa was achieved on 26 October 1972 in Munich. The prototypes were used to test some of the concepts in what was to become the Panavia Tornado programme, including 'fly-by-wire' technology.

VAK191B from above
VAK191B from above

It was similar in concept to the British Harrier, but was designed for a supersonic dash capability (Mach 1.2-1.4) at medium to high altitudes. It was judged that having a single engine would create too much drag, but the two lift engines were dead weight in cruise, and the small cruise engine gave a poor thrust to weight ratio. It also had very small highly loaded wings. By contrast, the Harrier had such a high thrust to weight ratio, it was effective as a dogfighter, and had larger wings which were put to good use in rolling short takeoffs.

An example can be seen at the Deutsches Museum at Schleißheim near Munich.

Contents

[edit] Specification

rotating nozzle detail
rotating nozzle detail
  • Gross takeoff weight: 8507 kg (19,845 lb)
  • Length 16.40 m (53 ft 7 in)
  • Height 4.30 m (14 ft 1 in)
  • Wingspan: 6.16 m (20 ft 3 in)
  • Wing area: 19 m²
  • Empty weight: 5,562 kg
  • Gross weight (MTOW?) 9,000 kg (19,845 lb)
  • Service ceiling: 15,000 m
  • Range: 400 km
  • Max speed: 684 mph
  • 1 × Rolls Royce/MTU RB 193-12 with 45.2 kN (10,150 lbf) thrust
  • 2 × Rolls Royce RB 162-81 F 08 with 26.5 kN (5587 lbf) each[1]

[edit] References

  1. ^ X-Planes and prototypes Jim Winchester Barnes & Noble books

[edit] External links

[edit] See also

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