In numbers Through the lens Video
NATO reporting name: SS-N-25 Switchblade
Αlso known as: Izdeliye 78, "3M24"
Entered service: 2003
Designed to destroy surface war-ship with a displacement of up to 5.000 t.
Unified for use from the following platforms:
- Uran-E shipborne missile system
- Bal-E land-based mobile missile system
- tactical and naval aviation combat aircraft, as well as surveillance fixed-and rotary-wing aircraft.
Technical specifications
| DESIGNER | "Zvezda" Design buream, Tactical Missiles Corporation JSC |
| COUNTRY | Russia |
| TYPE |
Anti-ship missile
|
| Aircraft-bearer (aerial means) |
Su-30M, Su-35S, Su-34, MiG-29K
|
| Helicopter's-bearer (aerial means) |
Κa-27, Κα-28, Κα-52Κ
|
|
POWER-PLANT
|
Turbofan engine
|
|
Thrust, kgf
|
- |
|
DIMENSIONS
|
|
|
Length, m
|
5,7 |
| - naval version | 4,4 |
| - air version | 3,85 |
| Wing span, m | - |
| Fin span, m | - |
| Diameter, m | 0,42 |
|
WEIGHT
|
|
|
Maximum missile weight, kg
|
|
|
- naval version
|
620
|
|
- land-based version's launch weight, kg
|
620
|
|
- air / heliborne version's launch weight, kg
|
520 until 610
|
|
Warhead weight, kg
|
145
|
|
PERFORMANCE
|
|
|
Maximum speed, km/h
|
980 |
|
Permissible height of use of the missile, km
|
- |
|
Launch range, km
|
until 130 |
|
Minimum permissible missile launch range, km
|
- |
|
Permissible speed of the aircraft before using the missile, km/h
|
- |
|
Circular error probable, m
|
- |
|
Seeker
|
- |
|
Warhead type
|
High-explosive - penetrating |
|
Guidance system
|
Active radar (Inertial navigation system + global navigation satellite system + passive - active radar). |
Photos X-35E (Kh-35E)