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At a glance
Astra (missile)larger figure on 0 of 3
R-40 (missile)larger figure on 3 of 3
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]
IR guided
Single sourceConfiguration
| Specification | Astra (missile) | R-40 (missile) |
|---|---|---|
| Speed | Mk-1: Mach 4.5[source] | Mach 2.2-4.5[source] |
| Type | Beyond-visual-range air-to-air missile[source] | Long-range air-to-air missile[source] |
| Place of origin | India[source] | Soviet Union[source] |
| In service | 2019 ( 2019 ) –present[source] | 1970–present |
radar guided
Single source6.29 m (20 ft 8 in)(radar guided) - 5.91 m (19 ft 5 in) (IR guided)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Used by | Indian Air Force Indian Navy[source] | Soviet Union , Syria , Iraq[source] |
|---|
| Wars | 2025 India–Pakistan conflict[source] | Iran–Iraq War , Gulf War , Operation Southern Watch[source] |
|---|
| Designer | Defence Research and Development Laboratory ( DRDO )[source] | OKB-4 MR Bisnovatyi[source] |
|---|
| Manufacturer | Bharat Dynamics Limited[source] | Vympel[source] |
|---|
| Unit cost | Mk-1: ₹ 7−8 crore (US$−830,000)[source] | — |
|---|
| Produced | 2017 − Present[source] | 1960s–1995[source] |
|---|
| Variants | Mk-1 (Operational) Mk-2 (LSP) Mk-3 (Trial-phase) VL-SRSAM (Trial-phase)[source] | R-40R / R-40T, R-40RD / R-40TD, R-40RD1 / R-40TD1 (radar and IR models)[source] |
|---|
| Warhead | High-explosive pre- fragmented HMX / PU[source] | Blast fragmentation[source] |
|---|
| Detonation mechanism | Mk-1: Radio proximity fuze Mk-2: Optical proximity fuze[source] | Radar and active laser fuzes[source] |
|---|
| Engine | Mk-1: Solid-propellant rocket Mk-2: Dual-thrust pulsed rocket motor Mk-3: Solid Fuel Ducted Ramjet[source] | Solid-propellant rocket motor[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] | Inverse monopulse Semi-active radar homing (R-40RD) Infrared homing (R-40TD)[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-25 , MiG-31[source] |
|---|
| Designed | — | 1959[source] |
|---|
| Reported operators | — |
|
|---|