R-14 Chusovaya

GPTKB entity

Statements (57)
Predicate Object
gptkbp:instance_of gptkb:missile
gptkbp:country_of_origin gptkb:Soviet_Union
gptkbp:deployment gptkb:1961
gptkb:1980s
silo and mobile
gptkbp:design gptkb:Moscow_Institute_of_Thermal_Technology
gptkbp:design_date gptkb:1955
gptkbp:design_feature two-stage rocket
gptkbp:design_purpose nuclear deterrence
gptkbp:development 1955-1961
gptkbp:diameter 1.5 m
gptkbp:disbandment_date gptkb:1980s
gptkbp:engine_type gptkb:RD-214
gptkbp:first_flight gptkb:1959
gptkbp:fuel_type kerosene and liquid oxygen
gptkbp:guidance_system 1,500 m
inertial navigation
inertial guidance system
gptkbp:has_limitations limited mobility
gptkbp:historical_significance Cold War deterrence strategy
https://www.w3.org/2000/01/rdf-schema#label R-14 Chusovaya
gptkbp:is_targeted_at inertial guidance
gptkbp:launch_date periodic tests
gptkbp:launch_platform gptkb:ground
mobile launcher
mobile launcher system
gptkbp:launch_site various sites in USSR
gptkbp:legacy influenced future missile designs
gptkbp:length 16.5 m
gptkbp:manufacturer gptkb:Moscow_Institute_of_Thermal_Technology
gptkbp:max_takeoff_weight 40,000 kg
gptkbp:military_branch gptkb:Strategic_Rocket_Forces
gptkbp:military_technology strategic nuclear strike
gptkbp:modifications upgraded guidance system
gptkbp:number_built approximately 100
gptkbp:operational_range 2,500 km
gptkbp:operational_status retired
gptkbp:operational_theater Europe and Asia
gptkbp:propulsion liquid propellant
100 k N
gptkbp:range 2,500 km
gptkbp:retired gptkb:1980
gptkbp:retirement gptkb:1980s
technological obsolescence
gptkbp:role strategic missile
gptkbp:service_entry gptkb:1961
gptkbp:status retired
gptkbp:successor gptkb:R-36_M
gptkb:R-36_missile
gptkbp:system gptkb:R-12_Dvina
gptkbp:used_by gptkb:Soviet_Armed_Forces
gptkbp:warhead_type thermonuclear
1.5 megatons
gptkbp:weight 40,000 kg
gptkbp:bfsParent gptkb:OKB-1
gptkb:Soviet_missiles_in_Cuba
gptkbp:bfsLayer 5