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Laister-Kauffman CG-10
Type of aircraft From Wikipedia, the free encyclopedia
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The Laister-Kauffman CG-10 was an American military transport glider aircraft developed during World War II.
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 of St. Louis, Missouri , 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]
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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
- Crew: 2
- Capacity: 42 troops / 2½-ton truck / two 105mm M2 howitzers / one M1 155 mm Long Tom howitzer / one M2 howitzer with a 1-ton 4 x 4 truck / 10,850 lb (4,921 kg) payload
- Length: 67 ft (20 m)
- Wingspan: 105 ft (32 m)
- Height: 26 ft 3.6 in (8.016 m)
- Cargo compartment:
- Length: 30 ft (9 m)
- Width: 8 ft 6 in (3 m)
- Height: 6 ft 8.4 in (2 m)
- Wing area: 1,180 sq ft (110 m2)
- Aspect ratio: 8.15
- Airfoil: root: NACA 23018; tip: NACA 4412[5]
- Empty weight: 12,150 lb (5,511 kg)
- Gross weight: 23,000 lb (10,433 kg)
Performance
- Stall speed: 75 mph (121 km/h, 65 kn) flaps up
- 62–70 mph (54–61 kn; 100–113 km/h) flaps down
- Never exceed speed: 180 mph (290 km/h, 160 kn)
- 140 mph (122 kn; 225 km/h) flaps down
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See also
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References
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