Engineering Division TW-1
Type of aircraft From Wikipedia, the free encyclopedia
The Engineering Division TW-1 was an American two-seat training biplane designed by the United States Army Engineering Division, only two were built and the type did not enter production.[1][2]
| TW-1 | |
|---|---|
| |
| Role | Training biplane |
| National origin | United States |
| Manufacturer | Engineering Division |
| First flight | 1920 |
| Primary user | United States Army Air Service |
| Number built | 2 |
Design and development
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Two prototypes of the TW-1 were built powered by a 230 hp (172 kW) Liberty 6.[1] The second aircraft was tested at McCook Field, (given the McCook designation P-200) and subsequently modified with a 350 hp (261 kW) Packard 1A-1237 engine but no others were built.[1]
Specifications
Data from [2]aerofiles.com
General characteristics
- Crew: 2
- Length: 28 ft 10 in (8.79 m)
- Wingspan: 41 ft 0 in (12.5 m)
- Powerplant: 1 × Liberty 6 , 230 hp (172 kW)
See also
Related lists
References
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