AMissiles
AIM-174B Gunslinger
Very long-range air-to-air missile Secondary air-to-ground and anti-ship missile roles (speculated)
Preparing your view.
AMissiles
Very long-range air-to-air missile Secondary air-to-ground and anti-ship missile roles (speculated)
At a glance
AIM-174B Gunslingerlarger figure on 4 of 4
Astra (missile)
Measured figures
Length
Single source16.5 ft (5.0 m)[source]
Length
Single sourceConfiguration
| Specification | AIM-174B Gunslinger | Astra (missile) |
|---|---|---|
| Type | Very long-range air-to-air missile Secondary air-to-ground and anti-ship missile roles (speculated)[source] | Beyond-visual-range air-to-air missile[source] |
| Place of origin | United States of America[source] | India[source] |
| In service | 2021 ( 2021 ) (?)–present; Testing may have begun as early as 2015[source] | 2019 ( 2019 ) –present[source] |
| Used by | United States Navy[source] |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
3.84 m (12.6 ft)[source]
AIM-174B · At least estimated to be beyond
Single sourceAIM-174B · Range
Single sourceOperational; +
Single source150–250 mi (240–400 km)+[source]
At least 150 mi (130 nmi; 241 km), estimated to be beyond 250 mi (217 nmi; 402 km)[source]
Operational; Mk-1
Single sourceOperational; Mk-2
Single sourceBars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Indian Air Force Indian Navy[source] |
| Manufacturer | Raytheon[source] | Bharat Dynamics Limited[source] |
|---|
| Warhead | High-explosive blast-fragmentation[source] | High-explosive pre- fragmented HMX / PU[source] |
|---|
| Detonation mechanism | Radar and contact/impact/proximity fuze[source] | Mk-1: Radio proximity fuze Mk-2: Optical proximity fuze[source] |
|---|
| Engine | Solid-fuel rocket motor[source] | Mk-1: Solid-propellant rocket Mk-2: Dual-thrust pulsed rocket motor Mk-3: Solid Fuel Ducted Ramjet[source] |
|---|
| Guidance system | Inertial guidance , terminal active and semi-active radar homing[source] | Mid-course: FOG - INS + Mid-course update via datalink Terminal: ARH[source] |
|---|
| Launch platform | Boeing F/A-18E/F Super Hornet[source] | Su-30MKI MiG-29K Tejas Mk.1/1A MiG-29UPG (Trial-phase) HAL Tejas Mk2 (Planned) AMCA (Planned) TEDBF (Planned) Rafale Marine (Planned)[source] |
|---|
| Airspeed | Up to Mach 3.5 (2,664.2 mph; 4,287.7 km/h; 1.2 km/s)[source] | — |
|---|
| Overall Weight | 1,830 lb (830.07 kg)[source] | — |
|---|
| Wars | — | 2025 India–Pakistan conflict[source] |
|---|
| Designer | — | Defence Research and Development Laboratory ( DRDO )[source] |
|---|
| Unit cost | — | Mk-1: ₹ 7−8 crore (US$−830,000)[source] |
|---|
| Produced | — | 2017 − Present[source] |
|---|
| Variants | — | Mk-1 (Operational) Mk-2 (LSP) Mk-3 (Trial-phase) VL-SRSAM (Trial-phase)[source] |
|---|
| Propellant | — | Solid fuel[source] |
|---|
| Flight ceiling | — | 20 km (66,000 ft)[source] |
|---|
Operational; Mk-3
Single sourceMk-1: 110 km (68 mi) Mk-2: 240 km (150 mi) Mk-3: 350 km (220 mi)[source]