In numbers Through the lens Video
NATO reporting name: -
Αlso known as: -
Entered service: -
GRAN - Mockup missile
High manoeuvrable guided air-to-air missile of the close air combat with infra-red homing head, non-contact radar target sensor in the millimeter range and controllable vector of the engine traction is intended for interception and destruction of the high manoeuv-rable means of aerial attack and reconnaissance under conditions of attack:
- at any time of twenty-four hours
- into forward and backward semispheres of the targets
- against ground, sky and water surface backgrounds
- under the ordinary and complex weather conditions
- with active informational and manoeuvrable counteraction of the enemy.
Missile is intended for use in the armament systems of the fighters, front bombers and low-flying attack aircrafts.
Technical specifications
| DESIGNER | State Kyiv Design Bureau "Luch" |
| COUNTRY | Ukraine |
| TYPE |
Guided air-to-air missile of close air combat
|
| Aircraft-bearer |
MiG-29 and others aircraft.
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DIMENSIONS
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| Length, m | 2,90 |
| Diameter, m | 0,165 |
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WEIGHT
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Maximum missile (launch) weight, kg
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60 |
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PERFORMANCE
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| Warhead type | Rod |
| Launch range, km | |
| - max at the front hemisphere | 40 |
| - min at the rear hemisphere | 20 |
| Minimum launch distance, km | |
| - at the front hemisphere | 0,65 |
| - at the rear hemisphere | 0,3 |
| Defeated targets g-load, g | 12 |
| Guidance system | Infrared (IR) |
| Fighter type target kill probability | 70 |
Photos GRAN Guided air-to-air missile of close air combat