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Astra (missile)

Indian beyond-visual-range air-to-air missile

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Through Aerodynamics

The missile will be integrated with the entire fighter fleet except the Dassault Mirage 2000 of the Indian Air Force as well as the Dassault Rafale fleet of the Navy. In 2024, the missile was cleared for full production.

Description

Astra Mark-1

Astra Mk-1 is 3.6 m (12 ft) long with a diameter of 178 mm (7.0 in) and weighs 154 kg (340 lb). It uses mid-course inertial guidance driven by fibre-optic gyroscope with terminal guidance through active radar homing. It is capable of receiving course corrections through a secure data link. The missile's active radar seeker, with a homing range of 25 km (16 mi), was originally designed by Russia's Concern Morinformsystem-Agat for the R-77 missile but manufactured within India. The seeker can lock-on to a target with a radar cross section of 5 square metres from a distance of 15 km and enables off-boresight launches up to an angle of 45°. Some tests in 2017 and 2018 validated an indigenous seeker replacing the earlier seeker. It is an improved active Ku, X band monopulse radio-frequency seeker developed by Research Center Imarat.

Astra Mk-1 is equipped with electronic counter-countermeasures to allow operation even during enemy attempts to jam the seeker using electronic countermeasures. It carries a 15 kg (33 lb) high explosive pre-fragmented warhead activated by a DRDO-developed laser proximity fuse. It uses a smokeless solid fuelled motor that can propel the missile to a speed of Mach 4.5 and allows operation from a maximum altitude of 20 km (66,000 ft). Its maximum range is 20 km (12 mi) in tail chase mode and 110 km (68 mi) in head-on chase mode. The maximum range is achieved when the missile launched from an altitude of over 15 km (49,000 ft). However, the maximum range of the missile when fired from an altitude of 8 km (26,000 ft) drops to 44 km (27 mi) and when launched from sea level, the range drops further to 21 km (13 mi). The seeker of the missile has a search range of 25 km (16 mi). The airframe can also handle up to 40g of lateral acceleration (latax). It can be launched in both autonomous and buddy mode operation and can lock on to its target before or after it is launched. The missile is designed for high off-boresight launches beyond 45°.

It can be launched in both autonomous and buddy mode operation and can lock on to its target before or after it is launched. The missile is designed for high off-boresight launches beyond 45°.

During an interview in January 2026, a DRDO official said the missile was fired from the LCA Tejas in 2025 where the target was detected at 140 km (87 mi) and was engaged at a range of 110 km (68 mi). The missile has already completed over 50 live firing trials. Further, the officials explained that following extensive feasibility talks between DRDO and Air Force officials after 2025 India–Pakistan conflict, the range of the existing missiles is being enhanced to 160 km (99 mi).

The Astra Mark-1 is offered to substitute for the R-77 on the Su-27, Su-30, Su-35, and MiG-29.

Astra Mark-2

The Astra Mk-2 has a maximum range of 130–160 km (81–99 mi) depending on the firing altitude. Multiple upgrades have been implemented including an in-house developed dual-pulse rocket motor, laser proximity fuze, fiber optic and gyroscope based Inertial navigation systems, two-way awacs datalink capability and an indigenous AESA radar seeker among others. As per reports in 2015, the expected maximum range of the missile was 150 km (93 mi) while featuring shorter fins.

It can be launched in both autonomous and buddy mode operation and can lock on to its target before or after it is launched. The missile is designed for high off-boresight launches beyond 45°.

According to an October 2025 report, the missile is now planned to have a maximum range of over 200 km. The propulsion system is modified for enhanced thrust is and trajectory shaping optimized to provide longer endurance. The missile will also reportedly incorporate technology from the Chinese-origin PL-15E missile that was recovered by the Indian forces in Hoshiarpur district, Punjab during 2025 India–Pakistan conflict and later studied by DRDO. The missile was recovered in a fully intact form due to a lack of self destruct technology.

The Defence Acquisition Council (DAC), chaired by Minister of Defence, cleared the range extension of Astra Mk 2 missiles for the Indian Air Force during its meet on 29 December 2025. During an interview in January 2026, a DRDO scientist said that the missile's range can be upgraded up to 240 km (150 mi) with the addition of a newly developed dual-pulse motor. The missile, with an indigenous content of 90%. is also expected to be integrated with the LCA Tejas. The missile will have two launch modes: hot launch, akin to the Mark 1 variant, and cold launch or ejection type launch.

Gandiva

The Gandiva missile, previously Astra Mark-3, incorporate an air-breathing propulsion system designated as Solid Fuel Ducted Ramjet setting it apart from the predecessors. By dimensions, the missile has a length of 3,838 mm (12.592 ft) and a diameter of 178–200 mm (7.0–7.9 in). This throttlable propulsion system significantly improves the range of the missile at 340 km (210 mi) at 20 km (66,000 ft) altitude and a range of 190 km (120 mi) at 8 km (26,000 ft) altitude. As per reports, the missile's launch speed ranges from Mach 0.8 to 2.2 while the target hit speed ranges from Mach 2.0 to 3.6. It can engage highly maneuverable fighter aircraft with high angle of attack of up to 20 degrees. With its "±10 km snap-up/snap-down capability" the missile allows the pilots to engage targets at both higher or lower altitudes with respect to the firing aircraft. The missile utilises a two-way data link for mid-course guidance from the launch aircraft or friendly AEW&C aircraft and also employs electronic counter-countermeasures.

VL-SRSAM

VL-SRSAM is based on Astra Mark 1 air-to-air missile with four short-span long-chord cruciform wings that provide aerodynamic stability. It also includes additional jet vane driven thrust vector control to enable quick reaction time on vertical launch and smokeless exhaust. VL-SRSAM conceived for area and point-defence role to save naval platforms. Each Vertical Launch System (VLS) can hold forty missiles in a twin quad-pack canister configuration carrying eight missiles each for hot launch that can be installed in an arrangement of multiple launch systems based on availability of space on the ship. The missile is for neutralizing various aerial threats at medium and close ranges, including fighter aircraft and sea skimming anti-ship missiles. With its 360° interception capability, as an integrated missile and weapon control system (WCS), it can identify and neutralize threats coming from all directions. Even though a short-range air defense missile was the original goal, the VL-SRSAM is a medium-range air defense system. Its attack range of 40 km has been increased to 80 km. The missile is said to be fitted in destroyers, frigates, corvettes and aircraft carriers.

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