SAF MIG-17
Soviet Air Force (SAF) MIG-17 "Frescoes"
The MIG-17 is a single seater high subsonic fighter developed by the mgyang Design Bureau of the Soviet Union in the late 1940s. The fighter is developed on the basis of MIG-15Bis. It adopts the conventional aerodynamic layout of swept wing, single engine, single seat, thrust weight ratio of 0.57, and is equipped with one 37mm machine gun and two 23mm machine guns. The maximum flight speed is 1100 km / h and the range is 2000 km.
MIG-17 fighter was designed in 1948, began test flight in December 1949, and entered the service of the former Soviet air force in 1952. There are many improved models of MIG-17, among which the most important type is mig-17f daytime fighter and MIG-17PF equipped with radar with all-weather combat capability.
A total of 10367 MIG-17 models were manufactured. In addition to production in the Soviet Union, China, Poland, the Czech Republic and other countries are also authorized to imitate mass production, so there are many derivative models. The MIG-17 was gradually retired and replaced by the supersonic MIG-19 fighter
ActivityGroup
AG1- H-37 37mm Gun
AG2- HP-23 23mm Gun
AG3-Discard the fuel tank
AG5-Parachute
AG6-Ejection seat escape
AG7-Light
AG8-Engine switch
Trim-Flap
Weapon
1* H-37 37 mm Gun
Number of clips:40
Ammunition change time:5s
Bullet velocity 6 RPS
2 HP-23 23 mm Gun
Number of clips:80
Ammunition change time:5s
Bullet velocity 9 RPS
Specifications
General Characteristics
- Created On Android
- Wingspan 34.9ft (10.6m)
- Length 33.9ft (10.3m)
- Height 14.3ft (4.4m)
- Empty Weight 6,129lbs (2,780kg)
- Loaded Weight 11,709lbs (5,311kg)
Performance
- Power/Weight Ratio 3.838
- Wing Loading 43.2lbs/ft2 (210.9kg/m2)
- Wing Area 271.1ft2 (25.2m2)
- Drag Points 4255
Parts
- Number of Parts 141
- Control Surfaces 7
- Performance Cost 640
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