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The BiPod, Rutan's latest design in association with his company Scaled Composites, is a hybrid flying car. Announced in July 2011, the twin-pod vehicle has a wingspan of 31 feet 10 inches; with the wings reconfigured (stowed between the pods), the car has a width of 7 feet 11 inches and fits in a single-car garage.
The Rutan VariEze is a composite, canard aircraft designed by Burt Rutan. It is a high-performance homebuilt aircraft , hundreds of which have been constructed. The design later evolved into the Long-EZ and other, larger cabin canard aircraft.
Scaled Composites was established in 1982 and purchased by the Beech Aircraft Corporation in 1985, as a result of the collaboration on the Starship project. In 1988, Beech's parent company, Raytheon, sold Scaled back to Rutan, who then sold it to Wyman-Gordon.
Wright Stagger EZ, a three-seat modification of the Rutan LongEZ. A Steve Wright three-seater design, using standard Long-EZ wings but with a dihedral canard and a rounder, more capacious fuselage. The pilot seat is standard Long-EZ, the co-pilot seat is offset to the right and 13" rearward, and behind the pilot seat is a third seat for a ...
The Rutan Model 77 Solitaire is an American, single seat, canard, mid-wing motor glider that was developed by Burt Rutan in response to the 1982 Sailplane Homebuilders Association Design Contest for a homebuilt glider. It first flew in 1982. [1]
“Dick never doubted whether my design would actually make it around, with still some gas in the tank,” Burt Rutan said. Voyager left from Edwards Air Force Base in California just after 8 a.m ...
The design was intended to replace the long-produced Bonanza. [1] The financial situation of Beech at the time, and competing projects, prevented consideration of commercial production. In 1988 Beechcraft sold Scaled Composites to the partnership of Rutan and the Wyman-Gordon Company , who also acquired the rights to a number of the designs ...
A design approach used by Burt Rutan is a high aspect ratio canard with higher lift coefficient (the wing loading of the canard is between 1.6 and 2 times the wing one) and a canard airfoil whose lift coefficient slope is non-linear (nearly flat) between 14° and 24°. [36] Another stabilisation parameter is the power effect.