In numbers Through the lens Video
NATO reporting name: -
Αlso known as: -
Entered service: 1974
The S-25L (S-25LD) missile is intended for attacking mobile and fixed armored targets, bunkers, tanks, and surface vessels.
It can be launched from low and medium altitudes under marginal weather conditions.
Technical specifications
| DESIGNER | "Zvezda" 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
|
Two-stage solid propellant rocket
|
|
Thrust, kgf
|
- |
|
DIMENSIONS
|
|
|
Length, m
|
- |
| Height, m | - |
| Wing span, m | - |
| Fin span, m | - |
| Diameter, m | - |
|
WEIGHT
|
|
|
Maximum missile weight, kg
|
286 |
| Warhead weight, kg |
108
|
|
PERFORMANCE
|
|
|
Maximum speed, km/h
|
1.062 |
|
Permissible height of use of the missile, m
|
- |
|
Launch range, km
|
up to 11 |
|
Minimum permissible missile launch range, km
|
- |
|
Permissible speed of the aircraft before using the missile, km/h
|
- |
|
Circular error probable, m
|
15 - 10 |
|
Seeker
|
- |
|
Warhead type
|
High-explosive |
|
Guidance system
|
Laser beams |