In numbers Through the lens Video
NATO reporting name: AS-14 Kedge
Αlso known as: 9-A-721
Entered service: 1990
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) |
Su-17M4, Su-24M Su-25, Su-34, Su-35, MiG-29SM, MiG-29SMT, MiG-29UTB, MiG-29K
|
|
POWER-PLANT
|
One-stage solid propellant rocket
|
|
Thrust, kgf
|
- |
|
DIMENSIONS
|
|
|
Length, m
|
3,90 |
| Width, m | - |
| Height, m | - |
| Wing span, m | 1,100 |
| Fin span, m | 0,750 |
| Diameter, m | 0,40 |
|
WEIGHT
|
|
|
Maximum missile weight, kg
|
700 |
| Warhead weight, kg |
320 (317)
|
|
PERFORMANCE
|
|
|
Maximum speed, km/h
|
- |
|
Permissible height of use of the missile, km
|
0,2 - 10 |
|
Launch range, km
|
20 - 30 (upgraded version) |
|
Minimum permissible missile launch range, km
|
3 - 4 |
|
Permissible speed of the aircraft before using the missile, km/h
|
600 - 1.250 |
|
Circular error probable, m
|
2 - 3 |
|
Seeker
|
- |
|
Warhead type
|
High-explosive - penetrating |
|
Guidance system
|
|
|
Combined with:
|
"Tubus-2" type passive TV guide head |
Photos X-29TE (Kh-29TE)
