il2_specs

CG-4A

描述

飞行构型的失速指示空速：65~86 km/h
俯冲极速：241 km/h
最大过载：3.5 G
飞行构型失速迎角：16°

起飞速度：86~113 km/h
进近速度：98~128 km/h
着陆速度：81~106 km/h
着陆迎角：8.0°

Optimal descent speed on glideslope: 2 m/s

注1：所提供的数据适用于国际标准大气（ISA）。
注2：飞行性能范围基于可能的飞机质量范围。

空重：1769 kg
最小重量：2383 kg
标准重量：3402 kg
最大起飞重量：4082 kg
有效载荷：2313 kg

长度：14.73 m
翼展：25.2 m
机翼面积：79.25 m²

首次投入战斗：1943年7月

操作特性：

• 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).

修改

漏斗形减速伞

安装减速伞以减少着陆滑行距离
增加重量：32 kg
预计速度降低：2 km/h

1000 kg货物

装载1000 kg军用物资
增加质量：1000 kg

13名伞兵

搭载13名全副武装的伞兵
增加质量：1415 kg

Willys MB

Willys MB 1⁄4 ton 4x4 utility truck
Additional mass: 1630 kg