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Contents

   



(Top)
 


1 Development  





2 Design  





3 Specifications (Defiant)  





4 References  














Rutan Defiant






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From Wikipedia, the free encyclopedia
 


Defiant
Rutan Defiant
Role Homebuilt aircraft
National origin America
Manufacturer Rutan Aircraft Factory
Designer Burt Rutan
First flight 30 June 1978

The Rutan Model 40 Defiant is a four-seat, twin-engine homebuilt aircraft with the engines in a push-pull configuration. It was designed by aerospace engineer Burt Rutan for the Rutan Aircraft Factory.

Rutan Defiant N57KS.
Rutan Defiant
An updated Defiant instrument panel with Dynon Avionics Skyview Efis
Defiant Taxi

Development[edit]

The prototype Defiant, N78RA, was first flown on 30 June 1978. It had been intended as a proof-of-concept of a very safe light twin design, requiring little trim change and no pilot action in case of engine failure, and with good single engine performance. A comparison of the Defiant single engine climb rate with a Gulfstream Cougar had shown about 390 feet (120 m) vs 280 feet (85 m) per minute at low altitude with both aircraft in a clean, gear up and flaps up, configuration. The prototype is now owned by the Hiller Aviation Museum.

In 1979 the Rutan Aircraft Factory announced they would proceed with certification of a Defiant-based light twin. Adequate financing was not secured for this project, and the design was modified for homebuilt construction as the Model 74, with the second aircraft (built by Fred Keller) appearing at Oshkosh 1983.[1] Plans were offered in mid-1984. 176 sets of plans were purchased before RAF discontinued selling plans in 1985.[2] Nine examples were known to be flying as of mid-1987. Nineteen are registered with the FAA as of 2005.

Design[edit]

The Defiant is built using fiberglass layup over Styrofoam core shapes in the same manner as the Rutan VariEze. The main gear is fixed, and there are no flaps. The Propellers are fixed-pitch non-feathering,[3] which is unusual in a twin-engine design. Cockpit entry is through a side hinged canopy.[1] The winglets provide yaw stability.[3] Unusually, the Defiant has a ventral, port offset, forward mounted rudder, as can be seen in pictures of the plane taxiing.

Specifications (Defiant)[edit]

General characteristics

Performance

References[edit]

  1. ^ a b Garrison, Peter (January 1984). "Doing the Defiant". Flying. New York, New York: Ziff-Davis. Retrieved October 17, 2014.
  • ^ Dan Linehan (2011). Burt Rutan's Race to Space: The Magician of Mojave and His Flying Innovations. Zenith Press. ISBN 978-0-7603-3815-5.
  • ^ a b Garrison, Peter (December 1978). "Rutan's Defiant". Flying. New York, New York: Ziff-Davis. Retrieved October 17, 2014.

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=Rutan_Defiant&oldid=1208453103"

    Categories: 
    Rutan aircraft
    1970s United States civil utility aircraft
    Twin-engined push-pull aircraft
    Canard aircraft
    Mid-wing aircraft
    Aircraft first flown in 1978
    Hidden categories: 
    Articles needing additional references from October 2011
    All articles needing additional references
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    This page was last edited on 17 February 2024, at 15:47 (UTC).

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