FORCETALLY
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Measured figures
Length
Single source9 feet 11 inches (3.02 m)[source]
Configuration
| Specification | AIM-9X Sidewinder | Sky Sword I |
|---|---|---|
| Speed | Mach 2.5+[source] | — |
| Type | short-range air-to-air missile[source] | Guided missile[source] |
| Place of origin | United States[source] | Taiwan[source] |
| Manufacturer | Raytheon[source] | National Chung-Shan Institute of Science and Technology[source] |
Wingspan
Single source11 in (279.4 mm)[source]
Operational; Operational range
Single source0.6 to 22 miles (1.0 to 35.4 km )[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.
| 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] | — |
|---|
| 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] | — |
|---|
| Cooling | internal cooling system[source] | — |
|---|
| In service | 1956–present[source] | 1980s to present[source] |
|---|
| Used by | See Operators[source] | Republic of China Air Force and Republic of China Army[source] |
|---|
| 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] | — |
|---|
| Warhead | WDU-17/B annular blast-fragmentation[source] | — |
|---|
| Detonation mechanism | IR proximity fuze[source] | — |
|---|
| Engine | Hercules/Bermite Mk. 36 solid-fuel rocket[source] | — |
|---|
| Launch platform | Aircraft, naval vessels, fixed launchers, and ground vehicles[source] | — |
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| Designed | — | Early 1980s[source] |
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| Variants | — | Antelope air defence system and Sea Oryx[source] |
|---|
| Role | — | short range infrared guided air-to-air missile[source] |
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| Reported operators |
| — |
|---|