| tiers | |
|---|
| categories | | "WEG" |
| "Cruise Missiles" |
| "Long-Range Cruise Missiles (LRCM) (More than 1,000 km)" |
| "Ground-Launched Cruise Missiles (GLCM) (More than 1,000 km)" |
| "Russia (RUS)" |
| "PRO_Russian Federation" |
| "Air" |
| "Tier1" |
|
|---|
| notes | "The Kh-101 / Kh-102 Raduga is a new line of conventional and nuclear-capable air-launched cruise missiles (ALCM) developed and deployed by Russia. A stealthy missile, the Kh-101 / Kh-102 is designed to defeat air defense systems by flying low and hugging the terrain to avoid their radar systems. The Kh-101 is the conventional warhead version while the Kh-102 is the nuclear-capable version of the Raduga.
The missile also has radar-absorbing capabilities which make it difficult to detect. It boasts a radar cross-section of .01 square meters.
The missile has no booster engine and therefore, relied on the altitude of its launch aircraft to assist it in reaching attack speed. The altitude window is 3,000m to 12,000m flying at a speed of 900km/h." |
|---|
| dateOfIntroduction | 1995 |
|---|
| countryOfOrigin | "Russia (RUS)" |
|---|
| proliferation | "Russian Federation" |
|---|
| selectedregions | |
|---|
| checkedregions | |
|---|
| checkedcountries | |
|---|
| dis | | name | "KH 101 CIS" |
|---|
| string | "02.06.222.001.057.000.000" |
|---|
|
|---|
| images | | "Kh-101-102.jpeg" |
| "Kh-101-102_on_cart.jpeg" |
| "Kh-101-Kh-102_image.jpeg" |
|
|---|
| sections | | name | "System" |
|---|
| properties | | name | "Alternate Designation" |
|---|
| value | "Kh-101; Kh-102" |
|---|
|
| name | "Class" |
|---|
| value | "Air Launched Cruise Missile" |
|---|
|
| name | "Effective Range" |
|---|
| value | "5,000 km (a source said that the range could be as high as 10,000 km)" |
|---|
|
| name | "Circular Error Probability" |
|---|
| value | "6" |
|---|
| units | "m" |
|---|
|
| name | "Basing" |
|---|
| value | "Tu-160 "Blackjack" (12 missiles), Tu-22M3/5 "Backfire" C (4 missiles), Tu-95M16 "Bear-H" (8 missiles), and Su-27IB (INA), Su-34 (2 missiles)" |
|---|
|
|
|---|
|
| name | "Dimensions" |
|---|
| properties | | name | "Length" |
|---|
| value | "7.45" |
|---|
| units | "m" |
|---|
|
| name | "Missile Weight" |
|---|
| value | "2,400" |
|---|
| units | "kg" |
|---|
|
| name | "Diameter" |
|---|
| value | "0.5" |
|---|
| units | "m" |
|---|
|
|
|
|---|
|
| name | "Payload" |
|---|
| properties | | name | "Warhead Options" |
|---|
| value | "Conventional and Nuclear" |
|---|
|
| name | "Warhead Type" |
|---|
| value | "Kh-101 = Conventional; Kh-102 = Nuclear" |
|---|
|
| name | "Warhead Weight" |
|---|
| value | "450" |
|---|
| units | "kg" |
|---|
|
| name | "Nuclear Yield" |
|---|
| value | "250" |
|---|
| units | "mT" |
|---|
|
| name | "Conventional Warhead Weight" |
|---|
| value | "400" |
|---|
| units | "kg" |
|---|
|
| name | "Conventional Warheads Available" |
|---|
| value | "HE, Fragmentation, Submunitions" |
|---|
|
|
|---|
|
| name | "Propulsion Characteristics" |
|---|
| properties | | name | "Engine" |
|---|
| value | "TRDD-50A Turbofan" |
|---|
|
| name | "Propellant" |
|---|
| value | "INA" |
|---|
|
| name | "Speed" |
|---|
| value | "900" |
|---|
| units | "km/h" |
|---|
|
| name | "Flight Ceiling" |
|---|
| value | "6,000" |
|---|
| units | "m" |
|---|
|
| name | "Minimum Flight Altitude" |
|---|
| value | "30" |
|---|
| units | "m" |
|---|
|
| name | "Cruise Altitude" |
|---|
| value | "30-70 m above the ground" |
|---|
|
| name | "Endurance" |
|---|
| value | "10" |
|---|
| units | "hours" |
|---|
|
|
|---|
|
| name | "Fire Control" |
|---|
| properties | | name | "Guidance System" |
|---|
| value | "Inertial, Electro-optical correction, GLONASS satellite navigation, and IR TV terminal guidance." |
|---|
|
| name | "Note:" |
|---|
| value | "For inflight course correction, the missile uses a pre-loaded map in its onboard computer to perform terrain comparison." |
|---|
|
|
|---|
|
|
|---|
| type | "WEG" |
|---|
| version | 1 |
|---|
