Wichita Engineering TG-10
| TG-10 | |
|---|---|
| Role | Glider |
| National origin | United States |
| Manufacturer | Wichita Engineering |
| Number built | 0 |
The Wichita Engineering TG-10 was a proposed American training glider conceived by Wichita Engineering in the early 1940s.
Design and development
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.[1]
Specifications
Data from [1]
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
References
- ^ a b Heyman, Jos (2015-02-01). "UNITED STATES MILITARY AIRCRAFT" (PDF). Retrieved 2023-10-16.
External links
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