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At a glance
Measured figures
Length
Single source9 feet 11 inches (3.02 m)[source]
PL-5B, PL-5C
Single sourceConfiguration
| Specification | AIM-9X Sidewinder | PL-5 |
|---|---|---|
| Speed | Mach 2.5+[source] | Mach 2.5[source] |
| Type | short-range air-to-air missile[source] | Short-range air-to-air missile[source] |
| Place of origin | United States[source] | China[source] |
| Manufacturer | Raytheon[source] |
PL-5E
Single source3.128 m (PL-5B, PL-5C), 2.893m (PL-5E)[source]
Warhead weight
Single source20.8 lb (9.4 kg)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Luoyang Electro-Optics Technology Development Centre (EOTDC), Hanzhong Nanfeng Machine Factory[source]
| Status | Its latest variants (AIM-9X) remain standard equipment in most Western-aligned air forces.[source] | — |
|---|
| Operators | USAF (the lead platform was the F-15C ) and the USN (the lead platform was the F/A-18C )[source] | — |
|---|
| Introduction | November 2003[source] | — |
|---|
| Guidance system | imaging infrared 128×128 element focal-plane array (FPA) seeker[source] | Infrared homing , multi-element, dual band detector(PL-5EII)[source] |
|---|
| Flight control | two-axis thrust-vectoring control (TVC) system[source] | — |
|---|
| Propulsion and warhead configuration | It retains the same rocket motor, fuze and warhead of the AIM-9M[source] | — |
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| Cooling | internal cooling system[source] | — |
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| In service | 1956–present[source] | — |
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| Used by | See Operators[source] | — |
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| Wars | Second Taiwan Strait Crisis Vietnam War Yom Kippur War Iran–Iraq War Gulf of Sidra incident (1981) Falklands War 1982 Lebanon War 1989 air battle near Tobruk Gulf War Bosnian War Operation Allied Force 2023 Chinese balloon incident Gaza war Red Sea crisis Russian invasion of Ukraine 2026 Iran War[source] | — |
|---|
| Unit cost | US$381,069.74 (Block II) US$399,500.00 (Block II Plus) US$209,492.75 (training missile) (All as of 2019 )[source] | — |
|---|
| Produced | 1953–present[source] | 1982[source] |
|---|
| Warhead | WDU-17/B annular blast-fragmentation[source] | 6kg blast-frag , or expanding rod (RF-fuse)[source] |
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| Detonation mechanism | IR proximity fuze[source] | Active infrared , laser proximity fuse(PL-5EII)[source] |
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| Engine | Hercules/Bermite Mk. 36 solid-fuel rocket[source] | Solid-fuel rocket[source] |
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| Launch platform | Aircraft, naval vessels, fixed launchers, and ground vehicles[source] | Aircraft, helicopter gunships[source] |
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| Reported operators |
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