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At a glance
Astra (missile)larger figure on 3 of 3
R-73 (missile)larger figure on 0 of 3
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Wingspan
Single source510 millimetres (20 in)[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]
Operational; R-73A, R-73E R-74
Single sourceOperational; RVV-MD
Single sourceR-73A, R-73E: 30 kilometres (19 mi) R-74, RVV-MD: 40 kilometres (25 mi)[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.
Configuration
| Specification | Astra (missile) | R-73 (missile) |
|---|---|---|
| Speed | Mk-1: Mach 4.5[source] | Mach 2.5[source] |
| Type | Beyond-visual-range air-to-air missile[source] | Short-range air-to-air missile[source] |
| Place of origin | India[source] | Soviet Union[source] |
| In service | 2019 ( 2019 ) –present[source] | 1984–present[source] |
| Used by | Indian Air Force Indian Navy[source] | See Operators[source] |
| Wars | 2025 India–Pakistan conflict[source] | Eritrean-Ethiopian War Yemeni civil war (2014-present) Russo-Ukrainian War[source] |
| Designer | Defence Research and Development Laboratory ( DRDO )[source] | — |
| Manufacturer | Bharat Dynamics Limited[source] | Moscow Kommunar Machine-Building Plant , Tbilisi Aircraft Manufacturing , TAM Management[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] | — |
| Warhead | High-explosive pre- fragmented HMX / PU[source] | 7.4 kilograms (16 lb)[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] | Solid-fuel rocket engine[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] | All-aspect infrared homing[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] | MiG-21 (Upgraded), MiG-23-98 , MiG-25 , MiG-27 , MiG-29 , MiG-31 , MiG-35 Sukhoi Su-24 , Su-25 , Su-27 , Su-30 , Su-33 , Su-34 , Su-35 , Sukhoi Su-57 , Sukhoi Su-47 Yak-141 , Yak-130 HAL Tejas IRIAF F-14 J-10 J-11 Mirage 2000 ( Indian Air Force ) MAGURA V5 USV ( HUR Ukraine ) 9K33 Osa Gravehawk[source] |
| Reported operators | — |
|