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Rutan VariViggen

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Homebuilt aircraft designed by Burt Rutan
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Rutan VariViggen
General information
TypeHomebuiltlight aircraft
ManufacturerRutan Aircraft Factory (plans supplier)
Designer
Status< 5 flying
Primary userprivate owners
Number built~20
History
First flightApril, 1972
VariantVariEze

TheRutan VariViggen is ahomebuilt aircraft designed byBurt Rutan. Theaircraft is a tandem two-seater of primarily wooden construction with adelta wing and acanard foreplane. The VariViggen is powered by a 150 hpLycoming O-320aero engine inpusher configuration. The prototype was designated Model 27, and the production version was Model 32.

Design and development

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The VariViggen was named after theSwedish fighter plane, theSaab 37 Viggen. This and theXB-70 Valkyrie inspired the design. Rutan became interested in aircraft which resistedstalls andspins, and the VariViggen was his first full scale design. He began working with the design as a student atCal Poly in the early 1960s, and started building the prototype in his garage in 1968. After four years of work, the aircraft made its first flight in April, 1972. In order to increase efficiency, the Model 32 (also known as the VariViggen SP) had a slightly longer fuselage, a larger wingspan and winglets.

TheRutan Aircraft Factory sold 600 plan sets for the VariViggen to homebuilders, and eventually about 20 of the aircraft were built. Following the crash of one inNew Brunswick,Canada in September 2006 due to wing tank fuel contamination,[1] fewer than five are currently still flying. The prototype aircraft, N27VV, can be seen in the 1975 movieDeath Race 2000 and was eventually donated to theEAA AirVenture Museum in 1988.

Rutan also began work on an all-aluminum variant, the MiniViggen, but later abandoned the project and focused his efforts on theVariEze.

VariViggen Model 27 Specifications (Standard Wing)

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Data from Jane's All the World's Aircraft 1976–77[2]

General characteristics

  • Crew: 1
  • Capacity: 1 passenger
  • Length: 19 ft 0 in (5.79 m)
  • Wingspan: 19 ft 0 in (5.79 m)
  • Wing area: 119 sq ft (11.1 m2)
  • Aspect ratio: 3.03
  • Empty weight: 950 lb (431 kg)
  • Max takeoff weight: 1,700 lb (771 kg)
  • Fuel capacity: 30 US gal (25 imp gal; 110 L) (Note: 5 US Gal Reserve).
  • Powerplant: 1 ×Lycoming O-320-A2A air-cooledflat-four, 150 hp (110 kW)
  • Propellers: 2-bladed Hegy wooden fixed-pitch, 5 ft 10 in (1.78 m) diameter

Performance

  • Maximum speed: 163 mph (262 km/h, 142 kn)
  • Cruise speed: 150 mph (240 km/h, 130 kn) 125mph (econ cruise at 7,000 ft (2,100 m))
  • Never exceed speed: 180 mph (290 km/h, 160 kn)
  • Range: 300–440 mi (480–710 km, 260–380 nmi) (max fuel, 30 minutes reserve).
  • Service ceiling: 14,000 ft (4,300 m)
  • Rate of climb: 800 ft/min (4.1 m/s)
  • Take-off run to 50 ft (15 m): 950 ft (290 m)
  • Landing run from 50 ft (15 m): 600 ft (180 m)

References

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  1. ^Aviation Investigation Report A06A0092, Transportation Safety Board of Canada, September 17, 2006
  2. ^Taylor 1976, p. 530

External links

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