Loading the evidence…
Preparing your view.
Preparing your view.

At a glance
Astra (missile)larger figure on 2 of 2
Hydra 70larger figure on 0 of 2
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source3.84 m (12.6 ft)[source]
Length
Single sourceConfiguration
| Specification | Astra (missile) | Hydra 70 |
|---|---|---|
| Type | Beyond-visual-range air-to-air missile[source] | Rocket[source] |
| Place of origin | India[source] | United States[source] |
| In service | 2019 ( 2019 ) –present[source] | — |
| Used by | Indian Air Force Indian Navy[source] | See Users[source] |
| Wars | 2025 India–Pakistan conflict |
41.7 in (1,060 mm)[source]
Operational; Mk-1
Single sourceOperational; Mk-2
Single sourceOperational; Mk-3
Single sourceMk-1: 110 km (68 mi) Mk-2: 240 km (150 mi) Mk-3: 350 km (220 mi)[source]
Effective; Effective firing range
Single sourceMaximum; Maximum firing range
Single sourceWarhead weight
Single source15 kg (33 lb)[source]
Muzzle velocity
Single source2,300 feet per second (700 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Designer | Defence Research and Development Laboratory ( DRDO )[source] | — |
|---|
| Manufacturer | Bharat Dynamics Limited[source] | General Dynamics[source]Current manufacturer · aktuell |
|---|
| Unit cost | Mk-1: ₹ 7−8 crore (US$−830,000)[source] | $2,799[source] |
|---|
| Produced | 2017 − 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] | — |
|---|
| 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] | — |
|---|
| 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] | unguided[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] | OH-58 Kiowa , UH-60 Black Hawk , MH-6 Little Bird , UH-1 Iroquois UH-1N Twin Huey UH-1Y Venom AH-1 Cobra , AH-1W SuperCobra , AH-1Z Viper , AH-64 Apache , Eurocopter Tiger , T-129 ATAK , OV-10 Bronco , A-10 Thunderbolt II , AV-8B Harrier II , F-16 Fighting Falcon , F/A-18 Hornet , P-3 Orion , Mi-24[source] |
|---|
| Reported operators | — |
|
|---|