title: Laister-Kauffman CG-10
text: # Laister-Kauffman CG-10
  
  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. 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.
  
  ## Specifications (XCG-10A)
  
  Data from Fighting Gliders of World War II, United States Military Aircraft: CG = Transport Glider (1941-1955), Popular Science February 1945 : What's New in Aviation
  
  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 $m^2)$
  * Aspect ratio: 8.15
  * Airfoil: root: NACA 23018; tip: NACA 4412
  * 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
  