In numbers Through the lens Video
NATO reporting name: AS-7 Kerry
Αlso known as: -
Entered service: 1974
X-23L (kh-23L) - is a version derived from the X-23, X-23M (Kh-23, Kh-23M) missile with a laser beam guidance system. In various publications it is referred to not as X-23L (Kh-23L), but as X-25L (kh-25L).
Technical specifications
| DESIGNER | "Zvezda-Strela" Design buream, Tactical Missile Corporation JSC |
| COUNTRY | Russia |
| TYPE |
Air-to-surface missile
|
| Aircraft-bearer (aerial means) |
MiG-23, MiG-27, Su-24, Su-25, Yak-38
|
|
POWER-PLANT
|
Solid propellant rocket
|
|
Thrust, kgf
|
- |
|
DIMENSIONS
|
|
|
Length, m
|
3,525 |
| Width, m | - |
| Height, m | - |
| Wing span, m | 0,785 |
| Fin span, m | - |
| Diameter, m | 0,275 |
|
WEIGHT
|
|
|
Maximum missile weight, kg
|
287 |
| Warhead weight, kg |
111
|
|
PERFORMANCE
|
|
|
Maximum speed, km/h
|
2.880 |
|
Permissible height of use of the missile, km
|
- |
|
Launch range, km
|
10 |
|
Minimum permissible missile launch range, km
|
- |
|
Permissible speed of the aircraft before using the missile, km/h
|
- |
|
Circular error probable, m
|
10 - 15 |
|
Seeker
|
- |
|
Warhead type
|
High-explosive |
|
Guidance system
|
Radio command guidance |