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gptkbp:instanceOf
|
cruise missile
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gptkbp:aircraft
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gptkb:Tu-160
gptkb:Tu-95MS
Tu-22M3
|
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gptkbp:deployedTo
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air-launched
|
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gptkbp:designedBy
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
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gptkbp:developer
|
estimated at $1 billion
|
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gptkbp:diameter
|
1 m
|
|
gptkbp:exportedTo
|
not exported
|
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gptkbp:firstAwarded
|
2015
|
|
gptkbp:firstFlight
|
conducted in 2011
|
|
gptkbp:firstIntroduced
|
2012
|
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gptkbp:guidedTours
|
within 10 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Kh-101
|
|
gptkbp:launched
|
up to 90 degrees
|
|
gptkbp:launchSite
|
strategic bombers
|
|
gptkbp:length
|
8.5 m
|
|
gptkbp:maxTakeoffWeight
|
about 1,500 kg
|
|
gptkbp:navigationEquipment
|
GLONASS
|
|
gptkbp:notableFeature
|
high accuracy
stealth capabilities
advanced guidance system
high survivability
multi-role capability
long range
high payload capacity
nuclear option available
low launch signature
reduced flight profile
|
|
gptkbp:operationalArea
|
strategic strikes
|
|
gptkbp:operationalRange
|
4500 km
|
|
gptkbp:operationalRole
|
strategic strike weapon
|
|
gptkbp:producedBy
|
gptkb:Tactical_Missiles_Corporation
|
|
gptkbp:productionCompany
|
2000s to 2012
|
|
gptkbp:propulsion
|
turbojet engine
|
|
gptkbp:provides
|
terminal guidance
inertial navigation system with GPS
|
|
gptkbp:range
|
up to 4500 km
|
|
gptkbp:relatedPatent
|
Kh-102
|
|
gptkbp:security
|
yes
low radar cross-section
|
|
gptkbp:speed
|
subsonic
|
|
gptkbp:status
|
in service
|
|
gptkbp:successor
|
gptkb:Kh-55
|
|
gptkbp:supportRole
|
gptkb:Syria
up to 3000 km
|
|
gptkbp:targets
|
land and naval targets
|
|
gptkbp:type
|
400 kg
conventional or nuclear
|
|
gptkbp:usedBy
|
gptkb:Russian_Armed_Forces
|
|
gptkbp:weight
|
about 1,500 kg
|
|
gptkbp:wingspan
|
8 m
|