In numbers Through the lens Video
NATO reporting name: AS-10 Karen
Αlso known as: Izdeliye 713
Entered service: 1981
Similar of the US AG-65E Maverick. The missile has the ability to hit targets likefixed and mobile targets, air defense systems, ships, aircraft on the ground, bridges, etc.
Technical specifications
| DESIGNER | "Zvezda" Design buream, Tactical Missile Corporation JSC |
| COUNTRY | Russia |
| TYPE |
Air-to-surface
|
| Aircraft-bearer (aerial means) |
MiG-23BN, MiG-23BM, MiG-27M, MiG-27K, MiG-27D, Su-17M2, Su-17M3, Su-17M4, Su-24M, Su-25, Su-25T, MiG-29M, Su-3S, Yak-141
|
|
POWER-PLANT
|
Two-stage solid propellant rocket
|
|
Thrust, kgf
|
- |
|
DIMENSIONS
|
|
|
Length, m
|
3,705 |
| Width, m | - |
| Height, m | - |
| Wing span, m | 0,755 |
| Fin span, m | 0,493 |
| Diameter, m | 0,275 |
|
WEIGHT
|
|
|
Maximum missile weight, kg
|
299 |
| Warhead weight, kg |
140
|
|
PERFORMANCE
|
|
|
Maximum speed, km/h
|
3.132 |
|
Permissible height of use of the missile, km
|
0,05 - 5 |
|
Launch range, km
|
10 |
|
Minimum permissible missile launch range, km
|
3 |
|
Permissible speed of the aircraft before using the missile, km/h
|
700 - 1.250 |
|
Circular error probable, m
|
6 or 10 |
|
Seeker
|
- |
|
Warhead type
|
High-explosive type F-27 |
|
Guidance system
|
SUR-73 with semiactive with inertial guidance lazer. |