Guided air-to-air missile of close air combat
- Details
- Category: Air weapons
PURPOSE
High manoeuvrable guided air-to-air missile of close air combat with infrared homing head, noncontact radar target sensor in millimetric range and thrust-vectoring engine is intended for interception and destruction of high manoeuvrable means of air attack and reconnaissance during assault:
- at any time of day or night;
- at the targets front and aft hemisphere;
- against ground, sky and water surface backgrounds;
- under ordinary and adverse weather conditions;
- with active informational and manoeuvrable counteraction of the enemy.
The missile is intended for use in armament systems of fighters, front bombers and low-flying attack aircrafts.
SPECIFICATIONS
| Carrier altitude, m | 20 – 20 000 |
| Target altitude, m | 20 – 20 000 |
| Carrier speed, km/h | 650 – 2 500 |
| Target speed, km/h | not more than 2 700 |
| Correlation of carrier and target speeds | 0,8 - 3,0 |
| Target overload, g | 0 – 12 |
| Target location above (under) carrier, m | 0 – 5 000 |
| Angles of target designation, …o | ±60 |
|
Maximum launch range under conditions of attack, km: - at aft hemisphere - at front hemisphere - at side aspect angles |
up to 20,0 up to 40,0 up to 15,0 |
|
Minimum launch range under conditions of attack, km: - at aft hemisphere - at front hemisphere - at side aspect angles |
0,30 0,65 0,60 |
| Time of guided flight, s | up to 25 |