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WWII American training glider
The
Wichita Engineering TG-10
was a proposed
American
training glider conceived by Wichita Engineering in the early 1940s.
Design and development
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The TG-10 was designed as a two-seat training glider with a side-by-side cockpit configuration. One aircraft was ordered on 25 June 1942 with the serial 42-57197. However, the contract was cancelled on 1 March 1943 before the aircraft was completed.
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Specifications
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Data from
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General characteristics
- Crew:
one
- Length:
25 ft 1 in (7.65 m)
- Wingspan:
50 ft 1 in (15.27 m)
Performance
- Maximum speed:
90 mph (145 km/h, 78 kn)
See also
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References
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External links
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USAAC/USAAF sequences (1924-1947)
| Assault Glider
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Bomb Glider
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Cargo Glider
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Fuel Glider
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Powered Glider
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Training Glider
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1948 USAF redesignations
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Tri-service sequence (1962-present)
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Not assigned
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