|National origin||United States|
|Primary user||United States Army Air Service|
Design and development[edit | edit source]
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[edit | edit source]
Data from aerofiles.com
- 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[edit | edit source]
References[edit | edit source]
Notes[edit | edit source]
Bibliography[edit | edit source]
- Andrade, John (1979). U.S. Military Aircraft Designations and Serials since 1909. Hinckley, Leicstershire, UK: Midland Counties Publications. ISBN 0-904597-22-9.
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