R-12 Dvina

GPTKB entity

Statements (55)
Predicate Object
gptkbp:instance_of gptkb:missile
gptkbp:architecture gptkb:OKB-155
gptkbp:associated_with Soviet missile development
gptkbp:associated_with_country gptkb:Russia
gptkbp:conflict Cold War tensions
gptkbp:decommissioned gptkb:1993
gptkbp:deployment gptkb:Eastern_Europe
1960s
mobile launchers
gptkbp:design_date gptkb:1955
gptkbp:design_influence Soviet missile design principles
gptkbp:diameter 1.2 m
gptkbp:engine_type liquid-fueled engine
gptkbp:era Cold War era
gptkbp:first_flight gptkb:1955
gptkbp:first_introduced gptkb:1959
gptkbp:fuel_type kerosene and nitric acid
gptkbp:guidance_system 1,000 m
inertial guidance
gptkbp:historical_context nuclear arms race
gptkbp:historical_significance gptkb:first_Soviet_road-mobile_ICBM
https://www.w3.org/2000/01/rdf-schema#label R-12 Dvina
gptkbp:influenced_by gptkb:German_V-2_rocket
gptkbp:is_influenced_by ballistic missile technology
gptkbp:launch_platform mobile launcher
mobile or silo
gptkbp:launched road-mobile
gptkbp:legacy foundation for future missile systems
gptkbp:length 8.4 m
gptkbp:manufacturer gptkb:Moscow_Institute_of_Thermal_Technology
gptkbp:max_takeoff_weight 4,200 kg
gptkbp:military_branch gptkb:Soviet_Army
gptkbp:notable_feature mobile launch capability
gptkbp:number_built over 1,000
gptkbp:operational_period 1959-1993
gptkbp:operational_range 2,000 km
gptkbp:operational_status retired
gptkbp:operational_use strategic deterrence
gptkbp:propulsion gptkb:liquid
gptkbp:range 2,000 km
gptkbp:related_to gptkb:Cold_War
gptkbp:retired gptkb:1993
gptkbp:retirement strategic arms reduction
gptkbp:retirement_year gptkb:1993
gptkbp:service_history gptkb:Soviet_strategic_missile_forces
gptkbp:significance gptkb:nuclear_weapons
gptkbp:status obsolete
gptkbp:successor gptkb:RT-2_PM_Topol
gptkbp:used_by gptkb:Soviet_Union
gptkbp:warhead_type nuclear or conventional
1.5 megaton
gptkbp:weight 4,200 kg
gptkbp:bfsParent gptkb:OKB-1
gptkb:Soviet_missiles_in_Cuba
gptkbp:bfsLayer 5