|
gptkbp:instanceOf
|
cruise missile
|
|
gptkbp:deployedTo
|
air-launched
|
|
gptkbp:design
|
long-range precision strike
low observable technology
|
|
gptkbp:designedBy
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:developer
|
gptkb:Russian_Ministry_of_Defense
|
|
gptkbp:engineType
|
turbojet engine
|
|
gptkbp:exportedTo
|
not exported
|
|
gptkbp:firstAwarded
|
Syria_conflict
|
|
gptkbp:firstFlight
|
2004
|
|
gptkbp:firstIntroduced
|
2012
|
|
gptkbp:guidedTours
|
high precision
|
|
gptkbp:hasArea
|
successful test flights
|
|
gptkbp:hasFieldOfUse
|
gptkb:Tu-160
|
|
gptkbp:historicalEvent
|
ongoing since 2000s
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Kh-101 missile
|
|
gptkbp:launchSite
|
gptkb:Tu-95MS
strategic bomber
aircraft launch
|
|
gptkbp:length
|
8.5 meters
|
|
gptkbp:manufacturer
|
gptkb:Tactical_Missiles_Corporation
|
|
gptkbp:maxTakeoffWeight
|
2,500 kg
|
|
gptkbp:militaryRank
|
gptkb:Russian_Air_Force
yes
|
|
gptkbp:navigationEquipment
|
inertial and satellite navigation
|
|
gptkbp:operationalArea
|
yes
|
|
gptkbp:operationalRange
|
5,500 km
|
|
gptkbp:operationalStatus
|
active
strategic targets
|
|
gptkbp:payloadCapacity
|
up to 1,000 kg
|
|
gptkbp:productionCompany
|
early 2000s
2000s to 2012
|
|
gptkbp:propulsion
|
turbojet engine
|
|
gptkbp:provides
|
within 10 meters
inertial navigation system with GPS
terrain contour matching
|
|
gptkbp:range
|
up to 5,500 km
|
|
gptkbp:security
|
yes
low radar cross-section
blended wing body
|
|
gptkbp:services
|
2012
|
|
gptkbp:speed
|
subsonic
|
|
gptkbp:strategicGoals
|
high
|
|
gptkbp:successor
|
Kh-102 missile
|
|
gptkbp:supportRole
|
yes
strategic strike weapon
up to 5,500 km
|
|
gptkbp:targets
|
active radar homing
land and naval targets
|
|
gptkbp:type
|
400 kg
nuclear or conventional
|
|
gptkbp:usedBy
|
gptkb:Russian_Armed_Forces
|
|
gptkbp:weight
|
2,500 kg
|
|
gptkbp:wingspan
|
8 meters
|