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China JH-7 Fighter Bomber

34.0k Akali  5.1 years ago
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Introduction:

The first double-engine, two-seat, supersonic, all-weather sniper bomber designed and developed by China in the 1980s. Designed and developed by China Aviation Industry Xi'an Aircraft Industry (Group) Co., Ltd. (code: 172 Factory) in cooperation with Aviation 603 Research Institute, it is mainly used for deep attack and marine and ground target attacks, and can be used for supersonic flight.

Technical characteristics:

Pneumatic structure

JH-7 adopts high standard double swept wing standard aerodynamic layout, using full-motion level Tail, single-sided vertical tail, belly deflector.

power system

The two turbofan-9 (WS-9) afterburner turbofan engines used in the JH-7 are produced under the permission of the British technology. The prototype is developed by Rolls-Royce for the F-4K/M fighter. "Sbee" Mk202 engine,

Control:

TRIM-Flaps

AG2-Discard the auxiliary fuel tank

AG3-Abandon bomb 50

Gallery:







Simple little work, I hope to like it!

General Characteristics

  • Successors 1 airplane(s)
  • Created On Windows
  • Wingspan 85.5ft (26.1m)
  • Length 108.0ft (32.9m)
  • Height 32.5ft (9.9m)
  • Empty Weight N/A
  • Loaded Weight 48,887lbs (22,175kg)

Performance

  • Power/Weight Ratio 3.033
  • Wing Loading 24.8lbs/ft2 (121.3kg/m2)
  • Wing Area 1,968.1ft2 (182.8m2)
  • Drag Points 39685

Parts

  • Number of Parts 692
  • Control Surfaces 4
  • Performance Cost 2,892