VFW / Fokker VAK 191B
1971
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VFW / Fokker VAK 191B

The VAK concept of NATO and the German Armed Forces required an aircraft that was able to take off from unprepared airfields without runways. Its mission was close air support. In addition it had to be able to fly long distances in extreme-low-altitude in order to prevent attacks of antiaircraft weapons and radar detection. Because of this the VAK was designed with short wings and a minor extension so it would provide its pilots a tolerable flight and bear aerodynamically difficult extreme-low-altitude-flights. The equipment was stored in a weapon bay.

The first prototype flew on September 10, 1971, the first transition - the transfer of vertical flight in horizontal and vice versa as well as turning off and on the lift-engines - was achieved on October 26, 1972 in Manching, Bavaria, at a speed of 400 km/h.

All three VAK 191B experimental aircraft completed a total of 91 flights that lasted all together 12 hours.

VFW / Fokker VAK 191B


Specification 
 MODELVAK 191B
 CREW1
 ENGINE1 x Rolls-Royce/MTU RB 193-12, 45.2kN + 2 x Rolls-Royce RB 162-81 F 08, 26.5kN
 WEIGHTS
    Take-off weight8507 kg18755 lb
    Empty weight5562 kg12262 lb
 DIMENSIONS
    Wingspan6.16 m20 ft 3 in
    Length14.72 m48 ft 4 in
    Height4.30 m14 ft 1 in
    Wing area12.5 m2134.55 sq ft
 PERFORMANCE
    Max. speed1100 km/h684 mph
    Cruise speed740 km/h460 mph
    Range400 km249 miles
 ARMAMENT2945kg of weapons

Comments 
David Williams, d.s.williams(@)gmx.net, 01.04.2008

Was the first transition really performed at a speed of 400 km/h? That seems highly unlikely to me.

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