gptkbp:instance_of
|
gptkb:Space_Launch_System
|
gptkbp:capacity
|
100,000 kg to LEO
|
gptkbp:crew_capacity
|
gptkb:0
|
gptkbp:debut
|
December 15, 1988
November 15, 1987
|
gptkbp:design
|
gptkb:Mikhail_Yangel
multi-stage rocket
|
gptkbp:development
|
gptkb:1980s
|
gptkbp:diameter
|
4.1 m
|
gptkbp:durability
|
no
|
gptkbp:engine
|
gptkb:RD-170
|
gptkbp:engine_type
|
gptkb:Team_Rocket
|
gptkbp:first_flight
|
gptkb:1987
gptkb:1988
|
gptkbp:has_programs
|
gptkb:Soviet_space_program
|
gptkbp:height
|
58.2 m
|
gptkbp:historical_significance
|
first heavy-lift rocket of the Soviet Union
|
https://www.w3.org/2000/01/rdf-schema#label
|
Energia
|
gptkbp:influenced_by
|
gptkb:N1_rocket
|
gptkbp:inspiration
|
gptkb:Saturn_V
|
gptkbp:launch_date
|
2
|
gptkbp:launch_event
|
100%
|
gptkbp:launch_mass
|
1,500,000 kg
|
gptkbp:launch_platform
|
gptkb:Baikonur_Cosmodrome
|
gptkbp:launch_price
|
estimated $170 million
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
gptkbp:launch_vehicle
|
heavy lift launch vehicle
Energia family
|
gptkbp:launch_window
|
limited to 1987-1988
|
gptkbp:manufacturer
|
gptkb:Soviet_Union
|
gptkbp:notable_features
|
high payload capacity
|
gptkbp:notable_mission
|
gptkb:Buran
|
gptkbp:number_of_stages
|
1 x RD-0120
4 x RD-170
|
gptkbp:operational_period
|
1987-1988
|
gptkbp:operational_status
|
retired
|
gptkbp:orbital_altitude
|
7.8 km/s
|
gptkbp:payload_capacity
|
100,000 kg
5.5 m diameter
satellites, space probes
|
gptkbp:payload_to_gto
|
20,000 kg
|
gptkbp:production_location
|
gptkb:Russia
|
gptkbp:propulsion
|
RP-1 and Liquid Oxygen
|
gptkbp:related_to
|
gptkb:Space_Shuttle
|
gptkbp:status
|
retired
|
gptkbp:strategic_goals
|
gptkb:0
|
gptkbp:success
|
2
|
gptkbp:successor
|
gptkb:Angara_rocket
|
gptkbp:technology
|
liquid-fueled rocket
|
gptkbp:third_stage_engines
|
1 x RD-0120
|
gptkbp:used_in
|
gptkb:Buran_program
|
gptkbp:bfsParent
|
gptkb:J._Balvin
gptkb:Buran
gptkb:Buran_program
gptkb:J_Balvin
gptkb:Buran_spacecraft
gptkb:astronaut
|
gptkbp:bfsLayer
|
4
|