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AIM-9 Sidewinder
IOC: 1956
AIM-9M-9 Sidewinder
Unitary Cost: USD$84,000
Also Known As
AIM-9M-8
Origin United States of America
Contractor/s
Raytheon
Applications
F-15C Eagle F-15D Eagle F-15E Strike Eagle F-16A Fighting Falcon F-16B Fighting Falcon F-16C Block 32 F-16C Block 40 F-16C Block 42 F-16C Block 50 F-16C Block 52 F-16C Fighting Falcon F-16D Block 32 F-16D Block 40 F-16D Block 42 F-16D Block 50 F-16D Block 52 F-16D Fighting Falcon F-16E Desert Falcon F-16F Desert Falcon F-16I Soufa F/A-18A Hornet F/A-18B Hornet F/A-18C Hornet F/A-18D Hornet
Family Members
AIM-9M Sidewinder AIM-9X Sidewinder
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Description:
The AIM-9 missile is a supersonic, heat-guided, air-to-air missile carried by most western fighter aircraft. It was introduced in 1956 (AIM-9B).
This missile is used for self-defense purposes in close range combat situation, less than 20 kilometers, also known as dogfight. Once the AIM-9 has been launched its seeker follows the heat signature of the enemy's aircraft engines. Current AIM-9 blast fragmentation warhead detonates by proximity.
The AIM-9M-9 Sidewinder missile is a derivative of the AIM-9M missile with expanded IR countermeasures detection capability.
Specifications
Dimensions: Diameter 120 mm, Length 2.9 m, Width 630 mm
Weights: Max Weight 86 kg (190 lb), Warhead 10 kg (22 lb)
Performance: Max Range 26,000 m (85,302 ft), Top Speed 850 mps (Mach 2.56)
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Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
Shaft-Horse-Power (shp)
Last Updated: Sunday, August 01, 2010
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