Astra | |
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Artist's image of Astra.
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Type | Air to Air Missile |
Place of origin | India |
Production history | |
Manufacturer | DRDO |
Produced | Pre Production/Testing |
Specifications | |
Weight | 154 kg |
Length | 3570 mm |
Diameter | 178 mm |
Warhead | 15 kg (33 lb) HE fragmentation directional warhead |
Detonation
mechanism |
Radar proximity fuse |
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Engine | Solid Fuel Rocket |
Wingspan | 254 mm |
Operational
range |
80-110 km in head on chase 20 km in tail chase |
Flight ceiling | 66,000 ft |
Speed | Mach 4.5+ |
Guidance
system |
Inertial, mid-course update and terminal active radar homing (15 km) |
Launch
platform |
Su-30MKI (ongoing trials). HAL Tejas (expected), Dassault Rafale (expected), HAL AMCA (expected) Sukhoi/HAL FGFA (expected), Mirage 2000 (expected) and MiG-29UPG (expected) |
Astra (Sanskrit: अस्त्र, Astra: Throwing weapon) is an active radar homing beyond-visual-range air-to-air missile (BVRAAM) developed by the Defence Research and Development Organisation (DRDO), India. Astra is designed to be capable of engaging targets at varying range and altitudes allowing for engagement of both short-range targets (up to 20 km) and long-range targets (up to 80-110 km) using alternative propulsion modes. Except for a failure in one test, the missile has successfully completed all its tests. The missile was last tested on 18 March 2015 from a Su-30MKI fighter against a simulated live target. Astra uses a smokeless propulsion system.
The missile guidance is provided by a terminal active radar-seeker and an updated mid-course internal guidance system, which locates and tracks targets. On-board electronic counter-measures jam radar signals from enemy radar, making tracking of the missile difficult. The performance characteristics of the missile are similar to the R-77RVV-AE (AA-12) and Super 530D, both currently used by the IAF. It is 3.8 metres long and is narrower in front of the wings. The propellant used is HTPB (solid-fuel). The warhead is a 15 kg HE (high-explosive) which is activated by a proximity fuse. The missile's maximum speed is Mach 4.5+ and can attain maximum altitude of 20 km. The missile can handle 40 g turns near sea level while attacking a manoeuvring target. Astra has ECCM features and has improved effectiveness in multi-target scenarios. It can be launched in both autonomous and buddy mode operation and can achieve lock-on on its target before or after it is launched.
DRDO started developing the beyond visual range air-to-air missile (BVRAAM) to arm the Indian Air Force's Mirage 2000H, MiG-29, Sea Harrier, Su-30MKI, MiG-21 Bison and HAL Tejas fighter aircraft. The missile uses an indigenous solid fuel propellant. A rocket/ramjet propulsion for improved range and enhanced kinematic performance, similar to that used in the Akash surface-to-air missile, is also being developed.