Astra MK-2
| Name | Astra MK II |
|---|---|
| Image | ![]() |
| Country of origin | India (DRDO/BDL) |
| Range | 140-160 km |
| Max altitude | Not known |
| Length | 3.84 m |
| Diameter | 190 mm |
| Fin span | Not known |
| Mass | 154 kg |
| Flight Duration | Not known |
| Warhead | HE Pre Fragmented |
| Max Speed | Not known |
| Propulsion | HTBP based smokeless propellant |
| Engine | Dual-pulse rocket motor |
| Detonation Mechanism | Optical proximity Fuse |
| Guidance | Inertial, mid-course update and terminal active radar homing (13 km) |
| Launch platform | Su-30 MKI, LCA-TEJAS, TEJAS MK1A |
| Service period | 2025-Present |
| Description | The Astra Mk 2 is an advanced beyond-visual-range (BVR) air-to-air missile developed by the Defence Research and Development Organisation (DRDO) in India. It represents a significant upgrade over its predecessor, the Astra Mk 1, boasting an extended range of over 160 kilometers. Equipped with an indigenous, highly advanced seeker and enhanced maneuverability, the Astra Mk 2 is designed to effectively engage and neutralize aerial targets, including fighter jets, drones, and cruise missiles, at extended ranges. This cutting-edge missile significantly enhances the Indian Air Force’s air combat capabilities, providing a crucial edge in modern aerial warfare. |
| Website | https://bdl-india.in/astra |
Disclaimer: This information is based on publicly available sources and should be considered for general knowledge purposes only.
