.jpg "AIM-9M Sidewinder Short-range air-to-air missile © Konstantinos Panitsidis")
In numbers Through the lens Video
In the spring of 1979 began the first series of tests for a new missile AIM-9, whici essentially is a modernized version of the AIM-9L.
Technical specifications
| DESIGNER | MTI, Hercules |
| COUNTRY | USA |
| TYPE |
Short-range air-to-air missile
|
| IN SERVICE |
1976
|
|
Aircraft-bearer (aerial means)
|
F-4E Phantom PI-2000, F-14, F-15, F-16, Tornado, Sea Harrier
|
|
Helicopters-bearer (aerial means)
|
Possibility of transport by helicopters
|
|
POWER-PLANT
|
Rocket engine
|
|
Thrust, kgf
|
- |
|
DIMENSIONS
|
|
|
Length, mm
|
2.830
|
| Diameter, mm | 127 |
|
Wing span, mm
|
530
|
|
Fin span, mm
|
- |
|
WEIGHT
|
|
|
Maximum missile weight, kg
|
75 |
| Warhead weight, kg |
11
|
|
PERFORMANCE
|
|
|
Maximum speed, km/h
|
3.062 |
|
Maximum range, km
|
18 |
|
Target g-load, g
|
- |
| Explosive weight, kg |
-
|
| Warhead type |
High-explosive
|
|
Guidance system
|
Infrared homing (IR) |
Photos AIM-9 Short-range air-to-air missile
