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DRDO Ballistic Missile Defence System

Developer

Defence Research and Development Organisation

Engine

Two stage

Flight Altitude

80km

Speed

Mach 5

Guidance System

Inertial Navigation System Ground-based mid-course correction Active radar homing (Terminal phase)

Launch Platform

8 x 8 Tatra TEL

Length

7.5m

Diameter

<0.5m

Weight

1,200kg

Engine

Single stage

Flight Ceiling

30km

Speed

Mach 4.5

Guidance System

Inertial Navigation System Mid-course update Active radar homing (Terminal phase)

Launch Platform

8 x 8 Tatra TEL

Mission Control Software

Defence Research and Development Laboratory

Navigation and Electromechanical Actuation Systems

The Research Centre, Imarat

Motors, Jet Vanes and Structure

Advanced System Laboratory

Propellants

High Energy Materials Research Laboratory
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