|
gptkbp:instanceOf
|
missile
|
|
gptkbp:associatedWith
|
gptkb:Cold_War
|
|
gptkbp:decommissioned
|
1980s
|
|
gptkbp:deployedTo
|
mobile
|
|
gptkbp:design
|
gptkb:OKB-155
1950s
|
|
gptkbp:designedBy
|
gptkb:Soviet_Union
|
|
gptkbp:developer
|
1959
|
|
gptkbp:diameter
|
1.5 m
|
|
gptkbp:energyEfficiency
|
yes
|
|
gptkbp:engine
|
100 kN
|
|
gptkbp:engineType
|
liquid rocket engine
|
|
gptkbp:firstDeployment
|
1961
|
|
gptkbp:firstFlight
|
1959
1970s
over 20
|
|
gptkbp:firstGeneration
|
1961
1980s
|
|
gptkbp:gameFeatures
|
liquid propellant
|
|
gptkbp:hasArea
|
Kapustin Yar
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-14M
|
|
gptkbp:launched
|
mobile command post
road-mobile
|
|
gptkbp:launchSite
|
mobile launcher
mobile launchers
|
|
gptkbp:length
|
16.5 m
|
|
gptkbp:manufacturer
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:maxTakeoffWeight
|
40,000 kg
|
|
gptkbp:numberBuilt
|
approximately 100
|
|
gptkbp:operationalArea
|
gptkb:Soviet_Armed_Forces
|
|
gptkbp:operationalRange
|
2000 km
|
|
gptkbp:payloadCapacity
|
1.2 megaton
|
|
gptkbp:primaryUser
|
gptkb:Soviet_Army
|
|
gptkbp:productionCompany
|
1955
|
|
gptkbp:provides
|
500 m
inertial navigation
inertial guidance
|
|
gptkbp:range
|
2000 km
|
|
gptkbp:relatedPatent
|
gptkb:R-12
R-12,_R-16
|
|
gptkbp:relatedTo
|
gptkb:R-12_missile
|
|
gptkbp:retired
|
1980s
|
|
gptkbp:retirementYear
|
1980s
|
|
gptkbp:services
|
1961
1980s
|
|
gptkbp:speed
|
gptkb:Mach_3
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
RT-2PM Topol
|
|
gptkbp:type
|
nuclear
ballistic missile
|
|
gptkbp:usedBy
|
gptkb:Soviet_Union
|