JH-7A
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4.1 years ago
The j-h-7 is a supersonic fighter bomber with two engines in tandem and two seats, which was designed and developed by China Aviation Industry Xi'an Aircraft Industry (Group) Co., Ltd. and aviation 603 Research Institute. It was successfully tested in 1988. The aircraft is mainly equipped with Chinese Navy aviation, mainly used for campaign depth attack and sea and ground target attack, and can carry out supersonic flight.
Description:
Control key 1: acceleration
Control key 2: Aiming
Control key 3: Missile
Control key 4: parachute
Control key 5: horizontal flight(VTOL can be used to control the flight status)
Control key 6: flap
Control key 7: ejection
Control key 8: gyroscope
Specifications
General Characteristics
- Successors 1 airplane(s)
- Created On Windows
- Wingspan 44.0ft (13.4m)
- Length 73.0ft (22.2m)
- Height 23.2ft (7.1m)
- Empty Weight 12,825lbs (5,817kg)
- Loaded Weight 38,870lbs (17,631kg)
Performance
- Power/Weight Ratio 2.081
- Wing Loading 13.9lbs/ft2 (67.6kg/m2)
- Wing Area 2,806.0ft2 (260.7m2)
- Drag Points 12772
Parts
- Number of Parts 604
- Control Surfaces 5
- Performance Cost 2,264
为什么排名这么低啊,不应该
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