| TW-1 | |
|---|---|
| |
| Role | Training biplaneType of aircraft |
| National origin | United States |
| Manufacturer | Engineering Division |
| First flight | 1920 |
| Primary user | United States Army Air Service |
| Number built | 2 |
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.
Design and development
 | This section needs expansion. You can help by adding to it. (April 2017) |
Two prototypes of the TW-1 were built powered by a 230 hp (172 kW) Liberty 6. 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.
Specifications
Data from 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
Notes
- ^ Andrade 1979, p. 171
- ^ "American airplanes: Ea - Ew". www.aerofiles.com. 2 May 2009. Retrieved 13 November 2011.
Bibliography
- Andrade, John (1979). U.S. Military Aircraft Designations and Serials since 1909. Hinckley, Leicestershire, UK: Midland Counties Publications. ISBN 0-904597-22-9.
| Engineering Division aircraft | |
|---|---|
| Bombers | |
| Two-seat fighters | |
| Single-seat fighters | |
| Trainers | |
| USAAS trainer designations 1919–1924 | |
|---|---|
| Trainer, air-cooled | |
| Trainer, water-cooled | |