FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Astra (missile)larger figure on 0 of 3
RUM-139 VL-ASROClarger figure on 3 of 3
Measured figures
Length
Single source3.84 m (12.6 ft)[source]
Length
Single sourceConfiguration
| Specification | Astra (missile) | RUM-139 VL-ASROC |
|---|---|---|
| Type | Beyond-visual-range air-to-air missile[source] | Anti-submarine missile[source] |
| Place of origin | India[source] | United States[source] |
| In service | 2019 ( 2019 ) –present[source] | 1993 – present[source] |
| Used by | Indian Air Force Indian Navy[source] | United States Navy , Japan Maritime Self-Defense Force and others |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
16 ft 1 in (4.89 m)[source]
Wingspan
Single source2 ft 3.4 in (696 mm)[source]
Warhead weight
Single source15 kg (33 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | 2025 India–Pakistan conflict[source] | — |
|---|
| Designer | Defence Research and Development Laboratory ( DRDO )[source] | Goodyear Aerospace[source] |
|---|
| Manufacturer | Bharat Dynamics Limited[source] | Lockheed Martin[source] |
|---|
| Unit cost | Mk-1: ₹ 7−8 crore (US$−830,000)[source] | — |
|---|
| Produced | 2017 − Present[source] | 1993 – present[source] |
|---|
| Variants | Mk-1 (Operational) Mk-2 (LSP) Mk-3 (Trial-phase) VL-SRSAM (Trial-phase)[source] | — |
|---|
| Warhead | High-explosive pre- fragmented HMX / PU[source] | RUM-139A: Mark 46 Mod 5 torpedo RUM-139B: Mark 46 Mod 5A(SW) torpedo RUM-139C: Mark 54 torpedo[source] |
|---|
| Detonation mechanism | Mk-1: Radio proximity fuze Mk-2: Optical proximity fuze[source] | — |
|---|
| Engine | Mk-1: Solid-propellant rocket Mk-2: Dual-thrust pulsed rocket motor Mk-3: Solid Fuel Ducted Ramjet[source] | Two- stage solid-fuel rocket[source] |
|---|
| Propellant | Solid fuel[source] | — |
|---|
| Flight ceiling | 20 km (66,000 ft)[source] | — |
|---|
| Guidance system | Mid-course: FOG - INS + Mid-course update via datalink Terminal: ARH[source] | Inertial guidance and Mk 210 Mod 0 Digital Autopilot Control subsystem[source] |
|---|
| Launch platform | Su-30MKI MiG-29K Tejas Mk.1/1A MiG-29UPG (Trial-phase) HAL Tejas Mk2 (Planned) AMCA (Planned) TEDBF (Planned) Rafale Marine (Planned)[source] | Mk 41 VLS[source] |
|---|
| Designed | — | 1983 – 1993[source] |
|---|
| References | — | Janes[source] |
|---|