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The Laister-Kauffman CG-10 was an American military transport glider aircraft developed during World War II.

CG-10
CG-10A
Role Transport Glider
Designer Laister-Kauffman
First flight 1943
Primary user USAAF
Number built 5

Design and development


The development version was known as XCG-10. This version could carry 30 troops. It was accepted on October 4, 1943. The first test tow flight took place on November 6, 1943. The second version, XCG-10A, increased seating capacity to 42 and added a rear loading door.[1][2] Cargo capacity was up to 6 short tons (5.4 t).

The production version, CG-10A, had an initial order of 990 with the intention of being used for the planned invasion of Japan. 90 were on the production line when the program was cancelled. Laister-Kauffman considered fitting the planes with two Pratt & Whitney R-1830-92 engines but this plan never came to fruition.[2]


Specifications (XCG-10A)


Data from Fighting Gliders of World War II,[3] United States Military Aircraft: CG = Transport Glider (1941-1955),[2] Popular Science February 1945 : What's New in Aviation[4]

General characteristics

  • Length: 30 ft (9 m)
  • Width: 8 ft 6 in (3 m)
  • Height: 6 ft 8.4 in (2 m)

Performance

62–70 mph (54–61 kn; 100–113 km/h) flaps down
140 mph (122 kn; 225 km/h) flaps down

See also


Related lists


Operators


 United States

References


  1. Norton, Bill. American Military Gliders of World War II: Development, Training, Experimentation, and Tactics of All Aircraft Types. Atglen, PA: Shiffer Publishing, Ltd. p. 210.
  2. Heyman, Jos. "United States Military Aircraft: CG = Transport Glider (1941-1955)" (PDF). p. 12. Retrieved 3 September 2018.
  3. Mrazek, James E. (1 January 1977). Fighting Gliders of World War II (1st ed.). London: St. Martin's Press. pp. 121–123. ISBN 978-0-312-28927-0.
  4. "What's New in Aviation". Popular Science. February 1945. p. 85. Retrieved 3 September 2018.
  5. Lednicer, David. "The Incomplete Guide to Airfoil Usage". m-selig.ae.illinois.edu. Retrieved 16 April 2019.



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