Name	Astra MK III
Image
Country of origin	India (DRDO/BDL)
Range	190 km (Launched from 8 km altitude) 340 km (Launched from 20 km altitude)
Max altitude	20 km
Length	3.838 m
Diameter	178 mm
Fin span	200 mm
Mass	220 kg
Flight Duration	Not known
Warhead	HE Pre Fragmented
Max Speed	Mach 4.0+ (Terminal phase)
Propulsion	Solid Fuel (Boron infused HTBP propellant)
Engine	Solid Fuel Ducted Ramjet
Warhead	15 kg, high explosive pre-fragmented HMX/PU
Warhead yield	Not known
Detonation Mechanism	Not known
Guidance	Mid-course: Two way data-link, fibre optic ring laser gyroscope based inertial navigation system Terminal: Ku band AESA active radar seeker
Launch platform	Su-30 MKI, LCA-TEJAS, TEJAS MK1A
Service period	In development
Description	The Astra Mk 3 is a beyond-visual-range air-to-air missile currently under development by India’s Defence Research and Development Organisation (DRDO). It is envisioned as a further advancement upon the Astra Mk 1 and Mk 2 , incorporating improvements in range, seeker technology, and overall performance. While specific details remain classified, it is expected to feature enhanced capabilities against a wider range of aerial threats, including highly maneuverable fighter aircraft and unmanned aerial systems. The Astra Mk 3 is likely to integrate advanced technologies such as improved electronic countermeasures and a more sophisticated propulsion system.
Website	https://bdl-india.in/astra

Disclaimer: This information is based on publicly available sources and should be considered for general knowledge purposes only.