|
gptkbp:instanceOf
|
cruise missile
|
|
gptkbp:debutYear
|
2012
|
|
gptkbp:deployedTo
|
air-launched
|
|
gptkbp:design
|
gptkb:Russia
long-range precision strike
low observable technology
|
|
gptkbp:designedBy
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:developer
|
gptkb:Russian_Ministry_of_Defense
|
|
gptkbp:electronic_warfare
|
used_in_Syrian_Civil_War
|
|
gptkbp:engineType
|
RD-500 turbojet engine
|
|
gptkbp:exportedTo
|
not exported
|
|
gptkbp:firstFlight
|
2012
successful
|
|
gptkbp:firstIntroduced
|
2012
|
|
gptkbp:golfingEvents
|
30,000 feet
|
|
gptkbp:hasFieldOfUse
|
gptkb:Tupolev_Tu-95MS
|
|
gptkbp:historicalEvent
|
ongoing since 2000
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Kh-101 cruise missile
|
|
gptkbp:launchSite
|
strategic bombers
aircraft launch
air-launched cruise missile system
|
|
gptkbp:length
|
8.0 meters
|
|
gptkbp:maxTakeoffWeight
|
1,500 kg
|
|
gptkbp:militaryRank
|
gptkb:Aerospace_Forces_of_the_Russian_Federation
yes
|
|
gptkbp:operationalArea
|
yes
|
|
gptkbp:operationalRange
|
5,500 km
|
|
gptkbp:operationalStatus
|
active
high
Middle_East
|
|
gptkbp:producedBy
|
gptkb:Tupolev
|
|
gptkbp:productionCompany
|
2000
2000-2012
|
|
gptkbp:propulsion
|
turbojet engine
|
|
gptkbp:provides
|
inertial navigation system with GPS
terrain contour matching
|
|
gptkbp:purpose
|
strategic bombing
|
|
gptkbp:range
|
up to 5,500 km
|
|
gptkbp:secondaryRole
|
strategic strike weapon
|
|
gptkbp:security
|
yes
high
low radar cross-section
|
|
gptkbp:speed
|
subsonic
|
|
gptkbp:status
|
in service
|
|
gptkbp:successor
|
gptkb:Kh-55_missile
|
|
gptkbp:supportRole
|
gptkb:Syria
up to 5,500 km
|
|
gptkbp:targets
|
land and naval targets
satellite guidance
active radar and infrared homing
|
|
gptkbp:type
|
400 kg
nuclear or conventional
|
|
gptkbp:usedBy
|
gptkb:Russian_Armed_Forces
|
|
gptkbp:weight
|
1,500 kg
|
|
gptkbp:wingspan
|
8.0 meters
|