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Very Short Range Air Defence System or VSHORAD is a man-portable infrared homing surface-to-air missile system designed to eliminate low altitude aerial threats like helicopters, unmanned aerial vehicles etc at close ranges.
VSHORAD missile system was designed and developed by Defence Research and Development Organisation's (DRDO) Research Center Imarat (RCI) with the goal of replacing older Igla M MANPADs from the Indian armed Forces.
Indian Army and Air Force are expected to collectively order a total of 1200 VSHORAD missile and 200 Launchers by the end of FY 25-26.
What makes the Indian VSHORAD different from MANPADS present around the world is the presence of miniaturized Reaction Control System which drastically improves its precision in the end game.
Source - Indian Army PSQR document for the DRDO
VSHORAD missile system was designed and developed by Defence Research and Development Organisation's (DRDO) Research Center Imarat (RCI) with the goal of replacing older Igla M MANPADs from the Indian armed Forces.
Indian Army and Air Force are expected to collectively order a total of 1200 VSHORAD missile and 200 Launchers by the end of FY 25-26.
What makes the Indian VSHORAD different from MANPADS present around the world is the presence of miniaturized Reaction Control System which drastically improves its precision in the end game.
Type | |
Place of Origin | India |
Service History | Developmental Trials Complete, Awaiting User Trials |
Used By |
|
Designer | Research Centre Imarat (DRDO) |
Manufacturer | Adani Defence and Aerospace |
Unit Cost | - |
Mass | 20.5 kg |
Length | 2.00 metres (6 ft 7 in) |
Diameter | 90 mm (3.5 in) |
Wingspan | 32 cm (13 in) |
Warhead | 2.0 kg Directed Energy Blast Fragmentation Warhead |
Detonation Mechanism | Adaptive proximity fuze, Impact |
Engine | Dual-thrust rocket motor |
Operational Range | 250 m – 7 km |
Flight Altitude | 10 m - 3,500 m (11,500 ft) |
Speed | Mach 2 (Average Speed Mach 1.5) |
Azimuth | 360° |
Elevation | -5° to +35° |
Guidence | Dual waveband infra-red Homing |
Shelf Life | 15 years (maintenance free) |
Launch Platform | Tripod, Shoulder Mounted MANPAD |
Deployment time | • Setup to Firing Mode - 5 min • Stand by to Firing Mode - 10 sec |
Special Features | Miniaturized Reaction Control System |
Operating Visibility | Minimum of 10 lumens |
Operating Altitude | Maximum 4500 m |
Operating Temperature | -20°C to 45°C |
Launcher Unit Reliability | Capable of firing minimum 350 missiles |
EOTS Range | 12 km |
EOTS Field of View | greater than 8 deg × 8 deg |
Power Supply | Reusable Battery with Minimum 300 discharge cycles |
Power Supply Operability | Operate for 4 hours without recharge |
System Reliability | Sustain Minimum 10 continuous engagements |
Source - Indian Army PSQR document for the DRDO