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At a glance
AGM-179 JAGMlarger figure on 1 of 4
PL-8 (missile)
Measured figures
Length
Single source70 in (1,778 mm)[source]
Length
Single sourceConfiguration
| Specification | AGM-179 JAGM | PL-8 (missile) |
|---|---|---|
| Speed | — | ≈ Mach 3.5[source] |
| Type | Air-to-surface missile[source] | Short-range air-to-air missile Surface-to-air missile (land-based version)[source] |
| In service | Achieved IOC March 1st 2022 with the U.S. Marine Corps[source] | 1988 to present[source] |
| Manufacturer | Lockheed Martin[source] | Xi'an Eastern Machinery Factory and CATIC[source] |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
2.95 m (9 ft 8 in)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Unit cost | US$319,000 (FY 2023)[source] | — |
|---|
| No. built | 26,319 (planned)[source] | — |
|---|
| Guidance system | Semi-active laser and millimeter-wave radar[source] | Passive infrared homing[source] |
|---|
| Launch platform | Helicopters and fixed-wing aircraft[source] | Aerial and ground[source] |
|---|
| National origin | United States[source] | — |
|---|
| Place of origin | — | China[source] |
|---|
| Used by | — | China[source] |
|---|
| Produced | — | PL-8A: 1988 to 1990’s[source] |
|---|
| Warhead | — | 11 kg (24 lb) high explosive[source] |
|---|
| Detonation mechanism | — | Impact / Proximity[source] |
|---|
| Engine | — | Solid rocket[source] |
|---|
| Propellant | — | Solid fuel[source] |
|---|
| Flight ceiling | — | 21 km (13 mi)[source] |
|---|
| Flight altitude | — | .5 km (0.31 mi) minimum[source] |
|---|