Engineering:Bede BD-3
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Revision as of 08:17, 9 July 2022 by imported>MainAI (correction)
Short description: American prototype aircraft
BD-3 | |
---|---|
Role | Homebuilt aircraft |
National origin | United States |
Manufacturer | Bede Corporation |
Designer | Jim Bede |
First flight | 1965 |
Status | Prototype only |
The Bede BD-3 is a prototype six passenger homebuilt aircraft.
Design and development
The BD-3 is a six place, low wing pusher configuration aircraft with tricycle landing gear. The aircraft is powered by two engines driving a single shrouded pusher propeller connected with V belts and overriding clutches. The aircraft uses STOL Boundary layer control devices. The fuselage was built using aluminum honeycomb. Bede intended to scale up a turboprop variant for 15 and 24 passengers. The BD-3 prototype was sold to the EAA AirVenture Museum,[1][2] although by 2013 it did not appear on the museum's list of aircraft owned.[3]
Variants
- Bede XBD-2
- Flying prototype - Twin Continental O-300
- BD-3
- Production model
Specifications (BD-3)
Data from Air Progress, Flying
General characteristics
- Crew: 1
- Capacity: 5 passengers
- Length: 30 ft 8 in (9.35 m)
- Wingspan: 38 ft 5 in (11.71 m)
- Height: 12 ft 4 in (3.76 m)
- Wing area: 192 sq ft (17.8 m2)
- Gross weight: 4,300 lb (1,950 kg)
- Fuel capacity: 116 U.S. gallons (440 L; 97 imp gal)
- Powerplant: 2 × Lycoming IO-540-B1A-5 horizontally opposed piston aircraft engine, 290 hp (220 kW) each
- Propellers: 3-bladed Hartzell - Aluminum
Performance
- Cruise speed: 260 kn (300 mph, 480 km/h)
- Stall speed: 36 kn (42 mph, 68 km/h)
- Range: 1,100 nmi (1,270 mi, 2,040 km)
- Service ceiling: 28,000 ft (8,500 m)
See also
References
- ↑ Air Progress: 31. November 1978.
- ↑ Flying Magazine: 105. Nov 1962.
- ↑ "Aircraft Collection". AirVenture Museum. http://www.airventuremuseum.org/collection/aircraft/. Retrieved 2013-12-23.
Original source: https://en.wikipedia.org/wiki/Bede BD-3.
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