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VFW Fokker H3

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Wingspan
  
8.7 m

Engine type
  
Allison Model 250

Length
  
7.37 m

First flight
  
March 15, 1971

VFW-Fokker H3 httpsd1k5w7mbrh6vq5cloudfrontnetimagescache

The VFW-Fokker H3 Sprinter was a single-engined experimental rotorcraft designed and built in West Germany. Two aircraft were produced by VFW-Fokker in the early 1970s, registered D-9543 and D-9544. Intended as the first of a family of tip-jet driven helicopters the two H3 prototypes flew briefly but the method of rotor propulsion was found to be unsuccessful for this size of aircraft. Due to a high rotor overspeed, they could perform jump take-offs to 280 feet (85 m) at a rate of 1,600 feet (490 m) per minute. An improved H4 variant was designed but not built.

Contents

Aircraft on display

Both aircraft have survived, D-9543 is currently on display at the Hubschraubermuseum Bückeburg with the other H3 thought to be in a private collection in Germany.

Specifications (H3)

Data from Jane's Pocket Book of Research and Experimental Aircraft, 1976.

General characteristics

  • Crew: One
  • Capacity: 2 passengers
  • Payload: 270 kg (595 lb)
  • Length: 7.37 m (24 ft 2.25 in)
  • Rotor diameter: 8.70 m (28 ft 6.52 in)
  • Height: 2.50 m (8 ft 2.43 in)
  • Max. takeoff weight: 968 kg (2,134 lb)
  • Powerplant: 1 × Allison 250-C18 turboshaft
  • Performance

  • Cruise speed: 250 km/h (155 mph)
  • Service ceiling: 4,000 m (13,120 ft)
  • References

    VFW-Fokker H3 Wikipedia


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