CG-4A
Description
Indicated stall speed in flight configuration: 65..86 km/h
Dive speed limit: 241 km/h
Maximum load factor: 3.5 G
Stall angle of attack in flight configuration: 16 °
Takeoff speed: 86..113 km/h
Glideslope speed: 98..128 km/h
Landing speed: 81..106 km/h
Landing angle: 8 °
Optimal descent speed on glideslope: 2 m/s
Note 1: the data provided is for international standard atmosphere (ISA).
Note 2: flight performance ranges are given for possible aircraft mass ranges.
Empty weight: 1769 kg
Minimum weight: 2383 kg
Standard weight: 3402 kg
Maximum takeoff weight: 4082 kg
Useful load: 2313 kg
Length: 14.73 m
Wingspan: 25.2 m
Wing surface: 79.25 m²
Combat debut: July 1943
Operation features:
- The glider is equipped with a towing mechanism with a detachable cable. The cable could be released upon command from the glider pilot, or from the pilot of the towing aircraft (by default, LShift+D).
- The airframe has interceptor spoilers with a manual mechanical drive, which, when released (by default, RAlt+B), reduce the lift of the wing and increase the drag, thereby shortening the glide path.
- The front part of the glider is a crew cabin, which on the ground can be tilted upward for loading and unloading cargo or troops.
- The aircraft has independent left and right pneumatic wheel brake controls. To apply either brake push the upper part of the rudder pedal.
- The airplane tailwheel rotates freely and does not have a lock.
- To provide shorter landing run drogue chute could be installed as modification. Maximum speed of drogue chute release (LAlt + D) is 225 km/h. After successfull landing and braking drogue chute should be jettisoned (LAlt + D).
Modifications
Braking Parachute
Installation of braking parachute for reducing the landing run distance
Additional mass: 32 kg
Estimated speed loss: 2 km/h
Cargo, 1000 kg
1000 kg of military cargo
Additional mass: 1000 kg
13 airborne troopers
13 airborne troopers with ammunition
Additional mass: 1415 kg
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Additional mass: 1630 kg