FORCETALLY
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At a glance
Measured figures
Length
Single source9.75 m (384 in)[source]
Minuteman III
Single sourceConfiguration
| Specification | Abdali-I | LGM-30G Minuteman III |
|---|---|---|
| Type | SRBM[source] | Intercontinental ballistic missile[source] |
| Place of origin | Pakistan[source] | United States[source] |
| Used by | Pakistan Army Army Strategic Forces Command[source] | — |
| Designer | SUPARCO (Rocket stage) DESTO (Warhead design/assembly)[source] | — |
| Designed | 1993–97 |
Minuteman III: 59.9 ft (18.3 m)[source]
Warhead weight
Single source500 kg (1,100 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Manufacturer | SUPARCO[source] | Boeing[source] |
|---|
| Warhead | Single conventional HE / ICM[source] | Minuteman III: 2–3 × W62 (retired), 2–3 × W78 (retired), 1 × W78 (active), or 1 × W87 (active)[source] |
|---|
| Transmission | Automatic[source] | — |
|---|
| Suspension | MAZ-7310 8WD (With Pakistani military markings)[source] | — |
|---|
| Propellant | Solid-propellent[source] | — |
|---|
| Guidance system | Inertial , Terminal[source] | — |
|---|
| Accuracy | 100 m (330 ft)—150 m (490 ft) CEP .[source] | — |
|---|
| Launch platform | Transporter erector launcher (TEL)[source] | — |
|---|
| Operators | — | United States Air Force[source] |
|---|
| In service | — | Minuteman III: 1970–present[source] |
|---|
| Guidance | — | gimballed inertial navigation system[source]Minuteman III (LGM-30G); navigation system The Guidance Replacement Program replaces the NS20A Missile Guidance Set with the NS50 Missile Guidance Set.[source]Minuteman III (LGM-30G); Guidance Replacement Program |
|---|
| Launch platforms | — | missile silos[source]Minuteman III; deployment described as of September 2017 |
|---|