.jpg "AIM-9 © Konstantinos Panitsidis")
Photos from the personal collection of Konstantinos Panitsidis
Technical specifications 
Photos 
Video
The missile, integrated into the arsenal of the USAF since 1977, is an improved version of theAIM-9E. The electronic circuits partially replaced by micro chips. It bears strongerservomichanisms control rudders and redesigned.
TECHNICAL SPECIFICATIONS
| LAUNCH-PLATFORM | F-4E Phantom PI-2000, F-14, F-15, F-16, Tornado, Sea Harrier, Hawk and Helicopters |
| DESIGNER | Hercules / Aerojet |
| IN SERVICE | 1977 |
| TYPE | Short-range air-to-air missile |
| POWER PLANT | Rocket motor |
| Thrust, kN | - |
| DIMENSIONS | |
| Length, mm | 2830 |
| Diameter, mm | 127 |
| Wing span, mm | 560 |
| WEIGHT | |
| Weight, kg | 78 |
| Warhead weight, kg | - |
| Warhead type | High-Explosive |
| GUIDANCE SYSTEM | Infrared homing |
| PERFORMANCE | |
| Speed, (Mach) | 2,5 |
| Range, km | 18 |
PHOTOS AIM-9J
