Engineering:Townsend Thunderbird
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Revision as of 14:32, 9 July 2022 by imported>Steve Marsio (update)
| Townsend Thunderbird | |
|---|---|
| Role | Homebuilt aircraft |
| National origin | United States of America |
| Designer | Gid Townsend |
| First flight | 1956 |
| Number built | 1 |
| Developed from | BT-13 |
The Townsend Thunderbird is a homebuilt design created by the experienced cropduster Gid Townsend and built in 1956 with assistance of Curtis Pitts.[1]
Design
The Thunderbird is powered by a 245 hp (183 kW) Jacobs radial engine with a constant speed propeller. The horizontal stabilizer and aluminum wings are the outer panels of a Vultee BT-13 trainer. The engine cowl is from a Cessna UC-78. The fuselage is welded tubing with fabric covering. The landing gear is from a Cessna 180.[2]
Operational history
By 1974 the prototype was unflyable. The aircraft was later metalized, the turtledeck was removed, and it was converted to use a Wright R-975 radial engine.[3]
Specifications (Townsend Thunderbird)
Data from Experimenter
General characteristics
- Capacity: 2
- Length: 21 ft 2 in (6.45 m)
- Wingspan: 27 ft 5 in (8.36 m)
- Height: 6 ft 6 in (1.98 m)
- Wing area: 120 sq ft (11 m2)
- Empty weight: 1,800 lb (816 kg)
- Fuel capacity: 50 gal
- Powerplant: 1 × Wright R-975 radial, 450 hp (340 kW)
Performance
- Maximum speed: 210 kn (240 mph, 390 km/h)
- Cruise speed: 132 kn (152 mph, 245 km/h)
- Stall speed: 65 kn (75 mph, 121 km/h)
- Rate of climb: 1,500 ft/min (7.6 m/s)
References
- ↑ Experimenter. July 1957.
- ↑ "Townsend sidebar". http://aerofiles.com/townsend.html. Retrieved 7 April 2011.
- ↑ "AL HESSELGRAVE'S THUNDERBIRD A-1". Sport Aviation. September 1980.
External links
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