Bristol BX-200
| BX-200 | |
|---|---|
| Role | Two-seat homebuilt monoplane |
| National origin | United States |
| Designer | Uriel Bristol |
| First flight | 15 July 1986 |
| Number built | 1 |
|
| |
The Bristol BX-200 is an American two-seat cross-country homebuilt monoplane designed and built by Uriel Bristol for amateur construction from plans or kits.[1]
Design and development
The prototype registered N3UB first flew on 15 July 1986 and was a mid-wing monoplane with tubular steel fuselage and wooden wings. The prototype had a fixed conventional landing gear with a tailwheel and was powered by a 180 hp (134 kW) Lycoming O-360-A4A piston engine. The enclosed cockpit has two seats side-by-side and room for 50 lb (22.7 kg) of baggage.[1]
Specifications (Prototype)
Data from Jane's All the World's Aircraft 1989-90[1]
General characteristics
- Crew: 2
- Length: 5.31 m (17 ft 5 in)
- Wingspan: 6.10 m (29 ft 0 in)
- Height: 1.50 m (4 ft 11 in)
- Wing area: 8.36 m2 (90.0 ft2)
- Empty weight: 363 kg (800 lb)
- Gross weight: 612 kg (1350 lb)
- Powerplant: 1 × Lycoming O-360-A4A, 134 kW (180 hp)
Performance
- Maximum speed: 398 km/h (247 mph)
- Cruising speed: 352 km/h (219 mph)
- Range: 926 km (575 miles)
- Endurance: 2 hours 30 min
- Service ceiling: 6100 m (20000 ft)
- G limits: +6/-3
References
Notes
Bibliography
- Taylor, ed. (1989). Jane's All the World's Aircraft 1989-90. London, United Kingdom: Jane's Yearbooks. ISBN 0-7106-0896-9.
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