|
gptkbp:instanceOf
|
ballistic missile
|
|
gptkbp:battle
|
up to 3 megatons
|
|
gptkbp:built
|
approximately 200
|
|
gptkbp:conflict
|
Cold_War_tensions
|
|
gptkbp:debutYear
|
1962
|
|
gptkbp:decommissioningDate
|
completed by 1990s
|
|
gptkbp:deployedTo
|
road-mobile
|
|
gptkbp:design_feature
|
high mobility
two-stage design
|
|
gptkbp:diameter
|
1.5 meters
|
|
gptkbp:engineType
|
liquid-fueled engine
|
|
gptkbp:firstFlight
|
1961
conducted in 1961
|
|
gptkbp:frequency
|
1960s to 1980s
|
|
gptkbp:fuelType
|
liquid propellant
|
|
gptkbp:gameFeatures
|
kerosene and nitric acid
|
|
gptkbp:historical_significance
|
part_of_Cold_War_arsenal
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-14 Chusovaya
|
|
gptkbp:launched
|
vertical launch
capable of launching from various terrains
|
|
gptkbp:launchSite
|
various_sites_in_the_Soviet_Union
|
|
gptkbp:legacy
|
influenced future missile designs.
|
|
gptkbp:length
|
16.5 meters
|
|
gptkbp:manufacturer
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:maxTakeoffWeight
|
40,000 kg
|
|
gptkbp:militaryService
|
gptkb:Soviet_Strategic_Rocket_Forces
|
|
gptkbp:operational_status
|
limited operational use
deployed_in_Eastern_Europe
|
|
gptkbp:operationalRange
|
2,500 km
|
|
gptkbp:origin
|
gptkb:Soviet_Union
|
|
gptkbp:productionYears
|
1984
1950s to 1960s
|
|
gptkbp:provides
|
1,000 meters
inertial guidance system
|
|
gptkbp:range
|
2,500 km
|
|
gptkbp:releaseFormat
|
mobile launcher
|
|
gptkbp:releaseYear
|
1962
|
|
gptkbp:retirementYear
|
1980
technological obsolescence
|
|
gptkbp:status
|
retired
|
|
gptkbp:strategicGoals
|
enhanced_Soviet_nuclear_capabilities
|
|
gptkbp:successor
|
RT-2PM Topol
|
|
gptkbp:supportRole
|
strategic deterrence
|
|
gptkbp:targets
|
inertial navigation
|
|
gptkbp:team
|
OKB-586
|
|
gptkbp:technology
|
gptkb:R-12_Dvina
|
|
gptkbp:type
|
thermonuclear warhead
|
|
gptkbp:weight
|
40,000 kg
|