VL-SRSAM Information
| Name of the missile | VL-SRSAM |
|---|---|
| Developed by | Defence Research and Development Organisation (DRDO) |
| Type | Surface-to-Air missile |
| Guidance mechanism | Fibre-optic gyroscope based inertial guidance (mid-course) and active radar homing (terminal phase) |
| Capability | Lock on before launch (LOBL) and lock on after launch (LOAL) |
| Communication | Datalink for mid-course updates |
| Intended for | Replacement of Barak 1 surface to air missile system on Indian Navy warships and short range air defence system for Indian Air Force |
| Service history | In service (from 2022) |
| Used by | Indian Navy |
| Designer | Defence Research and Development Organisation |
| Manufacturer | Bharat Dynamics Limited |
| Specifications | |
| Mass | 154 kg (340 lb) |
| Length | 3.84 m (12.6 ft) |
| Diameter | 178 mm (7.0 in) |
| Warhead | High-explosive pre-fragmented HMX/PU[1] |
| Detonation mechanism | Radio proximity fuze |
| Engine | Solid-propellant rocket |
| Wingspan | 508 mm (20.0 |
VSHORAD Information
| Type | Short-range Air Defense (SHORAD) |
|---|---|
| Place of origin | India |
| In service | Under development |
| Designer | Research Centre Imarat (DRDO) |
| Manufacturer | Adani Defence and Aerospace |
| Mass | 20.5 kg (45 lb) |
| Length | 2.00 metres (6 ft 7 in) |
| Diameter | 90 mm (3.5 in) |
| Warhead | 2.0 kg (4.4 lb) |
| Detonation mechanism | Adaptive proximity fuze |
| Engine | Dual-thrust rocket motor |
| Wingspan | 32 cm (13 in) |
| Propellant | Solid propellant |
| Operational range | 250 m (820 ft) – 6 km (20,000 ft) |
| Flight altitude | 3,500 m (11,500 ft) |
| Maximum speed | Mach 1.5 |
| Guidance system | Dual waveband infra-red |
| Launch platform | Tripod, weapon platform |
Akash Missile Specifications
| Type | Medium range Surface-to-air missile system |
|---|---|
| Place of origin | India |
| In service | 2023 (planned) |
| Used by | Indian Air Force |
| Designer | Defence Research and Development Organisation |
| Designed | 2021 |
| Manufacturer | Bharat Dynamics Limited Bharat Electronics Limited Electropneumatics and Hydraulics India |
| Rate of fire | 1 missile in 10 seconds 3 missiles in 20 seconds |
| Warhead | Fragmentation |
| Detonation mechanism | Optical proximity fuze |
| Engine | Dual-pulse solid rocket motor |
| Propellant | Solid fuel |
| Operational range | 40–70 km (25–43 mi) |
| Flight altitude | 0.030–14 km (98-45,932 ft) |
| Guidance system | Mid-course: Inertial navigation system with two way datalink Terminal: Active radar homing |
XRSAM Information
| Specification | Details |
|---|---|
| Name | XR-SAM (eXtra-long Range Surface to Air Missile) |
| Developed by | Defence Research and Development Organization (DRDO) |
| Place of origin | India |
| Service history | In service 2024 (planned) |
| Warhead | Fragmentation |
| Detonation mechanism | Optical proximity fuze |
| Operational range | 350-400 km |
| Use against | 250 km against fighter jets, 350 km against cruise missiles, sea skimming anti-ship missiles, AWACS and mid air refuelers and will be capable of bringing down ballistic missiles and stealth fighters in the terminal stage. |
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