|
gptkbp:instanceOf
|
ballistic missile
|
|
gptkbp:associatedWith
|
gptkb:Intermediate-Range_Nuclear_Forces_Treaty
gptkb:Cold_War
|
|
gptkbp:decommissioned
|
1990s
|
|
gptkbp:deployedTo
|
gptkb:Eastern_Europe
1959
|
|
gptkbp:design
|
gptkb:MKB_Raduga
two-stage rocket
|
|
gptkbp:developedBy
|
gptkb:Soviet_Union
|
|
gptkbp:diameter
|
1.2 m
|
|
gptkbp:engineType
|
liquid rocket engine
|
|
gptkbp:exportedTo
|
various countries
|
|
gptkbp:firstFlight
|
1955
|
|
gptkbp:firstGeneration
|
1960
|
|
gptkbp:gameFeatures
|
liquid propellant
|
|
gptkbp:hasArea
|
numerous
|
|
gptkbp:historicalContext
|
nuclear arms race
|
|
gptkbp:historicalSignificance
|
first operational IRBM in USSR.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-12 Dvina
|
|
gptkbp:influenced
|
ballistic missile technology
|
|
gptkbp:influencedBy
|
V-2 rocket
|
|
gptkbp:inspiredBy
|
German_missile_technology
|
|
gptkbp:launched
|
road-mobile
|
|
gptkbp:launchSite
|
mobile launcher
mobile launchers
|
|
gptkbp:legacy
|
influenced future missile designs
|
|
gptkbp:length
|
8.4 m
|
|
gptkbp:maxTakeoffWeight
|
40,000 kg
|
|
gptkbp:militaryRank
|
gptkb:Soviet_Strategic_Rocket_Forces
nuclear deterrence
|
|
gptkbp:notableUsers
|
gptkb:Soviet_Armed_Forces
|
|
gptkbp:numberBuilt
|
over 1000
|
|
gptkbp:operationalRange
|
2000 km
|
|
gptkbp:operationalStatus
|
retired
|
|
gptkbp:origin
|
gptkb:Soviet_missile_program
|
|
gptkbp:payloadCapacity
|
1,000 kg
|
|
gptkbp:productionCompany
|
1950s
|
|
gptkbp:provides
|
1,000 m
inertial guidance
|
|
gptkbp:range
|
2000 km
|
|
gptkbp:relatedTo
|
gptkb:R-14_Chusovaya
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:retirementYear
|
1990
strategic arms reduction
|
|
gptkbp:significance
|
first Soviet IRBM
|
|
gptkbp:speed
|
gptkb:Mach_3
|
|
gptkbp:status
|
obsolete
|
|
gptkbp:strategicGoals
|
deterrent capability
|
|
gptkbp:successor
|
gptkb:SS-20_Saber
RT-2PM Topol
|
|
gptkbp:supportRole
|
strategic deterrence
|
|
gptkbp:type
|
1,000 kg
nuclear
|
|
gptkbp:usedBy
|
gptkb:Warsaw_Pact
|