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
|