UR-500

GPTKB entity

Statements (53)
Predicate Object
gptkbp:instance_of gptkb:Team_Rocket
gptkbp:configuration two-stage
gptkbp:control_system inertial guidance
gptkbp:country_of_origin gptkb:Soviet_Union
gptkbp:design gptkb:Vladimir_Chelomey
10 years
multi-stage
gptkbp:development 1960s
OKB-456
gptkbp:development_cost gptkb:unknown
gptkbp:diameter 3.8 meters
gptkbp:engine_type liquid-fueled
gptkbp:environmental_impact gptkb:unknown
gptkbp:first_flight gptkb:1967
gptkbp:fuel_type kerosene and liquid oxygen
gptkbp:height 60 meters
https://www.w3.org/2000/01/rdf-schema#label UR-500
gptkbp:influenced_by gptkb:R-7_Semyorka
gptkbp:inspired_by gptkb:Vostok_rocket
gptkbp:intended_use gptkb:Space_Launch_System
gptkbp:launch_date planned monthly
gptkbp:launch_mass 300,000 kg
gptkbp:launch_price gptkb:unknown
gptkbp:launch_site gptkb:Baikonur_Cosmodrome
gptkbp:launch_vehicle Proton family
gptkbp:launched gptkb:0
gptkbp:manufacturer gptkb:Moscow_Institute_of_Thermal_Technology
gptkbp:mass 250,000 kg
gptkbp:number_of_engines gptkb:5
gptkbp:number_of_stages gptkb:RD-0210_engine
gptkb:RD-0211_engine
RD-250 engine
gptkbp:operational_period 1967-1970
gptkbp:payload_capacity 4 meters
20,000 kg
gptkbp:projected_commercial_use gptkb:none
gptkbp:projected_end_of_service gptkb:1975
gptkbp:projected_historical_significance low
gptkbp:projected_international_collaboration gptkb:none
gptkbp:projected_launch_sites Baikonur, Plesetsk
gptkbp:projected_mission_types scientific, military
gptkbp:projected_payload 30,000 kg to GTO
gptkbp:projected_reusability gptkb:none
gptkbp:projected_technological_advancements gptkb:none
gptkbp:propulsion 1,000 k N
gptkbp:public_interest low
gptkbp:purpose heavy-lift launch vehicle
gptkbp:related_to gptkb:Soviet_space_program
gptkbp:safety_record gptkb:unknown
gptkbp:status canceled
gptkbp:successor gptkb:Proton_rocket
gptkbp:bfsParent gptkb:Chelomey_design_bureau
gptkbp:bfsLayer 6