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Engineering Division TW-1
Type of aircraft From Wikipedia, the free encyclopedia
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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]
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Design and development
![[icon]](#/media/File:Wiki_letter_w_cropped.svg){kind=small} | 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.[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
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References
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