ASTRA (Beyond Visual Range Air to Air Missile)

ASTRA is a BVR (Beyond Visual Range Air to Air) class missile with proven flight range of 85+ km. The missile is configured with diameter of 178 mm and length of 3838 mm. Its launch mass is 170 kg. The missile can be fired using rail type launcher. It is equipped with mid-course inertial guidance system followed by terminal homing guidance. The mid-course guidance is carried out on the basis of target updates received via data link. The RF seeker provides large autonomous range for terminal phase. The missile is equipped with high accuracy proximity fuse and fragmented type warhead to ensure high kill probability. Integration of ASTRA missile with Su-30MKI has been carried out successfully. The missile system is platform independent and it can be integrated with other aircraft.

Application of the Product

Anti-Aircraft Air to Air Missile

HELINA (Air to Ground Missile)

• Lock-On-Before-Launch (LOBL)
• Fire & Forget’ and ‘Top Attack’ Capability
• Day & Night Operation Capability
• Homing Guidance with Imaging Infra-Red (IIR) Seeker
• Warhead - HEAT
• Min - Max Range - (500 m, 7000 m)
• Platform - Advanced Light Helicopter (ALH)
• Operating Altitude - Sea Level to 6 km
• Launch Height - 10 m to 50 m above ground level
• Length : 1.9 m
• Diameter : 0.16 m
• Weight : 46.5 kg
• Speed : 240 m/s
• Range : 500 m to 7 km
• SSKP : >80%

Application of the Product

Indian Defence forces

LRSAM (Long Range Surface to Air Missile)

• Length : 4.5 m
• Diameter : 0.225 m
• Weight : 284 kg
• Range : 1 to 70 km
• Altitude : 16 km (Max)
• Speed : Mach 3
• Propulsion - Dual Pulse Solid Propellant Rocket Motor.
• Guidance - Midcourse INS with course correction with Radar data, and Terminal Active Seeker.
• Warhead - Pre-fragmented High Energy (23 kg).
• Targets - Aircraft, sub sonic and Supersonic Cruise Missile and Helicopters.
• Single Shot Kill Probability: 0.8

Application of the Product:

Air Defence Missile based weapon system to neutralize aerial targets up to a range of 70Km. System is operational with three Indian Armed Forces (Navy, Air Force & Army )

Man Portable Anti-Tank Guided Missile(MPATGM) Weapon System

Range : 200 m to 2.5 km
Accuracy : 90 %
Guidance : IIR Seeker
Missile Weight : < 15 kg
Launcher Weight : < 15 kg
Diameter : 120 mm
Warhead : 650 mm RHA
Launch Mode : Man Portable
Life : 10 Years

Application of the Product

MPATGM is designed and developed as a 3rd Generation Fire-and-Forget missile for the Parachute, Parachute (Special Forces) and Infantry battalions of the Indian Army. It is intended to replace the MILAN system of France & Konkurs system of Russia in service with the Indian Army.

NAG (Third Generation Anti-Tank Guided Missile)

Lock-On-Before-Launch (LOBL)
‘Fire & Forget’ and ‘Top Attack’ Capability
Day & Night Operation Capability
High Performance Homing Guidance with Imaging Infra-Red Seeker
Potent Tandem Warhead –Effective Penetration in ERA Protected RHA of Enemy Tank
Min - Max Range: (500mtr, 4000mtr)
Missile Missile with Launch Tube
Length : 1.834m 1.9 m
Diameter : 0.158m 0.2 m
Weight : 44Kg 55Kg
NAG Missile is Deployed on BMP2k ICV based Vehicle called NAG Missile Carrier (NAMICA)

Application of the Product

Mechanized Forces, Indian Army

New Generation Anti-Radiation Missile (NGARM)

India’s first indigenous Anti-Radiation Missile for SEAD Mission Role

Application of the Product

Suppression of Enemy Air Defences by targeting ground based Surveillance and Fire Control Radars

QRSAM (Quick Reaction Surface to Air Missile)

Length : 4.4 m
Diameter : 0.225 m
Weight : 270 kg
Range : upto 30 km
Altitude : Up to 14 km
Propulsion : Solid Rocket Motor
Guidance
Mid Course - Inertial
Terminal Phase - RF Seeker
Warhead : Pre-fragmented

Application of the Product

• The Radars are four wall active array with capability of Search & Track on the move.
• Command & Control on the move.
• Radio & Satellite Communication on the move.
• Engagement of all Aerial Targets including low RCS targets.
• The Quick reaction time of weapon system for target engagement.

SFDR (Solid Fuel Ducted Ramjet)

Length : 3838 mm
Diameter : 178 / 200 mm
Altitude : SL - 20 km
Launch Mach No. : 0.8 - 2.0
Interception Mach No. : 2.0 - 3.6
Missile Launch Range : 190 km at 8 km altitude : 320 km at 20 km altitude
Angle of attack : 20o
Snap-up & snap-down : ±10km
Weight : 222+2 kg
Launch Platforms : SU 30, LCA
Guidance : Mid Course - Inertial (INS + Radar) Terminal - AESA Seeker

Brahmos MPM

The Microwave Power Module (MPS4053) is operating in a narrow bandwidth at X-band frequency with 200W RF Output. The MPM contain a short-length TWT and an SSPA in a cascaded mode, sharing the gain. A compact electronic power conditioner (EPC) powers the MPM which is designed to operate over a short period with natural cooling

Application of the Product

Missile seeker

STAR (Supersonic TARget)

Range : 55 - 175 km
Altitudes : 10 - 10000 m
Speed : 1.8 - 2.5 Mach
Flight Time : 50 - 200 s
RCS : 0.2 - 1.9 m2 (S,C,X,Ku)
Latax (g) : 3 g at 10 km
Payload : Miss Distance Indicator
Launch Platform : Ship/Ground
Shelf Life : 10 Years
Temp Bracket : +5 to +55o
• Catapult Launch System
• Liquid Ramjet