In numbers Through the lens Video
NATO reporting name: AS-9 Kyle
Αlso known as: -
Entered service: 1973
Technical specifications
| DESIGNER | MBK Raduga |
| COUNTRY | Russia |
| TYPE |
Anti radar missile
|
| Aircraft-bearer (aerial means) |
Su-17M3, Su-17M2, Su-17M, Su-24, Yak-28N, Tu-22M
|
|
POWER-PLANT
|
Two-stage liquid-propellant rocket
|
|
Thrust, kgf
|
- |
|
DIMENSIONS
|
|
|
Length, m
|
5,97 |
| Width, m | - |
| Height, m | - |
| Wing span, m | 1,39 |
| Fin span, m | - |
| Diameter, m | 0,450 |
|
WEIGHT
|
|
|
Maximum missile weight, kg
|
690 - 720 |
| Warhead weight, kg |
until 155
|
|
PERFORMANCE
|
|
|
Maximum speed, km/h
|
3.186 |
|
Permissible height of use of the missile, km
|
- |
|
Launch range, km
|
until 110 |
|
Minimum permissible missile launch range, km
|
- |
|
Permissible speed of the aircraft before using the missile, km/h
|
- |
|
Circular error probable, m
|
20 |
|
Seeker
|
- |
|
Warhead type
|
High-explosive 9A283 or fragmentation |
|
Guidance system
|
|
|
Combined with:
|
Passive radar PRG-28M |