In numbers Through the lens Video
NATO reporting name: AS-14 Kedge
Αlso known as: Izdeliye 63
Entered service: 1980
Designed to defeat visible hard-to-hit ground and above-water targets. Intended to arm fighters and strikers.
Technical specifications
| DESIGNER | "Molniya", "Vympel" Design buream |
| COUNTRY | Russia |
| TYPE |
Air-to-surface missile
|
| Aircraft-bearer (aerial means) |
MiG-27M, MiG-27D, MiG-27K, MiG-29M, Su-17M2, Su-17M3, Su-17M4, Su-24M, Su-25, Su-25T, Su-34/35
|
|
POWER-PLANT
|
One-stage solid propellant rocket
|
|
Thrust, kgf
|
- |
|
DIMENSIONS
|
|
|
Length, m
|
3,87 (3,90) |
| Width, m | - |
| Height, m | - |
| Wing span, m | 1,100 |
| Fin span, m | 0,750 |
| Diameter, m | 0,38 - 0,40 |
|
WEIGHT
|
|
|
Maximum missile weight, kg
|
660 |
| Warhead weight, kg |
317 (320)
|
|
PERFORMANCE
|
|
|
Maximum speed, km/h
|
2.700 |
|
Permissible height of use of the missile, m
|
0,2 - 5.000 |
|
Launch range, km
|
8 - 10 |
|
Minimum permissible missile launch range, km
|
2 - 10 |
|
Permissible speed of the aircraft before using the missile, km/h
|
600 - 1.250 |
|
Circular error probable, m
|
3,5 - 4 |
|
Seeker
|
- |
|
Warhead type
|
High-explosive - penetrating |
|
Guidance system
|
|
|
Combined with:
|
Semiactive laser guidance |