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Wichita Engineering TG-10

From Wikipedia, the free encyclopedia
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

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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.[1]

Specifications

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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

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References

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  1. ^ a b Heyman, Jos (2015-02-01). "UNITED STATES MILITARY AIRCRAFT" (PDF). Retrieved 2023-10-16.
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