| engagement of aerial targets | upto the speed of Zero to 500 m/s and altitude more than 6 km at maximum range of the missile
|
| Maximum Range |
Not less than 15 km
75 km for Mark-II variant
|
| salvo | 12 rockets in less than 45 seconds
|
| Crossover Range | Not less than 9 km.
|
| Altitude | Not less than 6 Km.
|
| Target Speed | 0 to 500 m/s
|
| Target | Missile should be able to engage hovering helicopters.
|
| Guidance | Suitable guidance system (with active and/or passive seekers).
|
| Warhead | Should cause destruction/incapacitation of the air target.
|
| SSKP | Not less than 70% with single missile and not less then 85% for a salvo of two missiles.
|
| Reaction Time | 6 seconds or less (from launch command for missile to launch of missile).
|
| Features |
ability to fire a salvo of more than two missiles and simultaneously control/guide the salvo of missiles
ability to carry out surveillance and tracking while on the move and immediately fire the missile on halting
Capable of tracking targets at speeds of zero to 500 m/s at an altitude of more than 6 Km
Availability of ECCM facility to support operational EW environment
Capability to control two or more missiles simultaneously
Appropriate tracking range to ensure engagement of aerial targets at maximum range of missile
equipment can move a distance of 50 Km cross country in a day with on board fuel tank and in addition be able to operate for eight hours in a day without refueling
capable of transportation by rail on broad gauge rakes of Indian Railways
capable of being operated in plains, deserts, semi-deserts terrain obtaining in India
auxiliary or trailer/vehicle mounted external power supply system for training, undertaking repairs and maintenance
|
