3M24
Initial Operational Capability (IOC) : 1983
Total Production : ?
Model | Status | Year | Produced |
---|---|---|---|
3M24 | Active | 1983 | ? |
Kh-35U | Active | 1994 | ? |
Kh-35UE | Active | 2012 | ? |
3M24
Group : Anti-Ship Missiles
Status : Active
Also Known As : 3M24E (export designation), SS-N-25 Switchblade, Uran
Origin : Russia
Initial Operational Capability (IOC) : 1983
Total Production : ?
The 3M24 is a subsonic, long range, sea-skimming anti-ship missile. It features a solid fuel booster, a turbojet powerplant, a high-precision radio-altimeter, and an active radar guidance system in the terminal phase of the flight. During the flight the Kh-35 missile depends on the radio-altimeter and the Inertial Navigation System (INS). The Kh-35 is the Soviet counterpart to US Harpoon missile.
The 3M24, SS-N-25 Switchblade NATO-codename, was designed to provide anti-ship capability for surface vessels. The Uran system consists of 16 3M24 missiles with two 8-cell sealed launchers.
Operators
Country | Status | State | Notes |
---|---|---|---|
![]() | Active | ? | |
![]() | Active | ? | |
![]() | Active | ? | |
![]() | Cancelled | ? | |
![]() | Active | ? | |
![]() | Active | ? | |
![]() | Active | ? | |
![]() | Active | ? |
Specifications
Notes | ||
---|---|---|
Number of Stages | 2 | |
Dimensions | ||
Diameter | 420 millimeter | |
Length | 3.8 meter | |
Wingspan | 930 millimeter | |
Mass | ||
Warhead | 150 kilogram | |
Weight | 630 kilogram | |
Performance | ||
Max Range | 130 kilometer | |
Min Range | 5,000 meter | |
Speed | ||
Cruise Speed | 0.80 mach |
Kh-35U
Group : Anti-Ship Missiles
Status : Active
Also Known As : 3M60, AS-20 Kayak, Kh-35E
Origin : Russia
Contractors : Tactical Missiles Corporation (KTRV)*, Radar MMS
Initial Operational Capability (IOC) : 1994
Total Production : ?
The Kh-35 is a subsonic, long range, sea-skimming anti-ship missile. It features a solid fuel booster, a turbojet powerplant, a high-precision radio-altimeter, and an active radar guidance system in the terminal phase of the flight. During the flight the Kh-35 missile depends on the radio-altimeter and the Inertial Navigation System (INS). The Kh-35 is the Soviet counterpart to the US Harpoon missile.
The Kh-35U, AS-20 Kayak NATO-codename, anti-ship missile has been designed to be released from fixed- and rotary-wing aircraft. It is a derivative of ship-launched 3M24 missile (Uran system).
Operators
Country | Status | State | Notes |
---|---|---|---|
![]() | Active | ? | |
![]() | Active | ? | |
![]() | Active | ? | |
![]() | Active | ? |
Specifications
Notes | ||
---|---|---|
Number of Stages | 2 | |
Dimensions | ||
Diameter | 420 millimeter | |
Length | 3.8 meter | |
Wingspan | 930 millimeter | |
Mass | ||
Warhead | 150 kilogram | |
Weight | 480 kilogram | |
Performance | ||
Max Range | 130 kilometer | |
Min Range | 5,000 meter | |
Speed | ||
Cruise Speed | 0.80 mach |
Kh-35UE
Group : Anti-Ship Missiles
Status : Active
Also Known As : AS-20 Kayak Mod 2
Origin : Russia
Contractors : Tactical Missiles Corporation (KTRV)*, Radar MMS
Initial Operational Capability (IOC) : 2012
Total Production : ?
The Kh-35UE is a subsonic, sea-skimming anti-ship missile designed to engage amphibious assault ships and cargo vessels navigating individually or as part of a convoy from longer ranges than the basic Kh-35 missile. Like its predecessor, the new missile can be released from both fixed- and rotary-wing aircraft. The helicopter version is longer and heavier than the airplane version (4.4 meters versus 3.85 meters and 650 kg versus 550 kg) but can be released at lower altitudes (100-3,500 meters) and airspeeds (0-0.25 Mach). The guidance system has been improved to make the missile system more effective against advanced targets.
The Kh-35UE features an improved propulsion system which doubles the effective range of the cruise missile from 130 km to up to 260 km. It features a high-precision radio-altimeter and an active radar guidance system in the terminal phase of the flight. During the flight the Kh-35UE missile depends on the radio-altimeter and the Inertial Navigation System (INS). It is fitted with a 145 High Explosive (HE) fragmentation, penetration warhead. The guidance system is resistant to electronic warfare jamming.
Operators
Country | Status | State | Notes |
---|---|---|---|
![]() | Active | ? | |
![]() | Active | ? | |
![]() | Active | ? | |
![]() | Active | ? |
Specifications
Notes | ||
---|---|---|
Number of Stages | 2 | |
Dimensions | ||
Diameter | 0.42 meter | |
Length | 3.9 meter | |
Wingspan | 1.3 meter | |
Mass | ||
Warhead | 145 kilogram | |
Weight | 660 kilogram | ship version, aircraft version 530 kg and helicopter version 630 kg |
Performance | ||
Max Cruising Flight Altitude | 15 meter | |
Max Launch Altitude | 10,000 meter | |
Max Range | 260 kilometer | |
Min Cruising Flight Altitude | 7 meter | |
Min Launch Altitude | 200 meter | |
Min Range | 7 kilometer | |
Sea-Skimming Flight Altitude | 4 meter | |
Seeker's Detection Range | 50 kilometer | |
Speed | ||
Cruise Speed | 0.85 mach | |
Max Launch Airspeed | 0.90 mach | |
Min Launch Airspeed | 0.35 mach |
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Notes
State Latest Known holdings/Original Procurement
Com - Date of Commissioning
Decom - Date of Decommissioning
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