gptkbp:instanceOf
|
cruise missile
|
gptkbp:deployedTo
|
strategic bomber aircraft
|
gptkbp:design
|
strategic strike
low-altitude flight
|
gptkbp:designedBy
|
gptkb:Soviet_Union
|
gptkbp:developer
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
gptkbp:engineType
|
RD-500
|
gptkbp:exportedTo
|
gptkb:Ukraine
|
gptkbp:firstIntroduced
|
1983
|
gptkbp:historicalSignificance
|
Cold War era weaponry
|
https://www.w3.org/2000/01/rdf-schema#label
|
Kh-55 cruise missiles
|
gptkbp:launched
|
10,000 meters
|
gptkbp:launchSite
|
aircraft
aircraft-mounted
air-launched
|
gptkbp:launchVehicle
|
Tu-95 bomber
|
gptkbp:length
|
8.3 meters
|
gptkbp:maxTakeoffWeight
|
1,200 kg
|
gptkbp:modifications
|
Kh-55SM, Kh-55SE
|
gptkbp:navigationEquipment
|
inertial and GPS
|
gptkbp:notableFeature
|
used in conflicts
|
gptkbp:notableUsers
|
gptkb:Russia
|
gptkbp:operationalArea
|
naval and land targets
|
gptkbp:operationalRange
|
2,500 km
|
gptkbp:operationalStatus
|
active
strategic military operations
|
gptkbp:payloadCapacity
|
400 kg
|
gptkbp:primaryUser
|
Russia,_Ukraine,_Kazakhstan
|
gptkbp:producedBy
|
gptkb:Moscow_Machine-Building_Plant
|
gptkbp:productionCompany
|
1970s to 1980s
|
gptkbp:propulsion
|
turbojet engine
|
gptkbp:provides
|
10-30 meters
inertial navigation system
terrain contour matching
|
gptkbp:range
|
2,500 km
|
gptkbp:relatedPatent
|
Kh-22
|
gptkbp:retirementYear
|
still in service
|
gptkbp:revenue
|
1980
|
gptkbp:security
|
yes
low radar cross-section
|
gptkbp:serviceHistory
|
used_by_Russia_and_other_countries
|
gptkbp:speed
|
0.8 Mach
|
gptkbp:status
|
in service
|
gptkbp:successor
|
gptkb:Kh-101
|
gptkbp:supportRole
|
gptkb:Gulf_War
2,500 km
strategic deterrence
|
gptkbp:targets
|
active radar homing
land and naval targets
|
gptkbp:technology
|
subsonic
|
gptkbp:type
|
nuclear or conventional
|
gptkbp:variant
|
gptkb:Kh-55SM
|
gptkbp:weight
|
1,200 kg
|
gptkbp:wingspan
|
8.0 meters
|