|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
3
|
|
gptkbp:bfsParent
|
gptkb:spacecraft
gptkb:J_Balvin
|
|
gptkbp:capacity
|
100,000 kg to LEO
|
|
gptkbp:crew
|
gptkb:0
|
|
gptkbp:debut_year
|
December 15, 1988
|
|
gptkbp:design
|
gptkb:Mikhail_Yangel
multi-stage rocket
|
|
gptkbp:developer
|
gptkb:1980s
|
|
gptkbp:diameter
|
4.1 m
|
|
gptkbp:durability
|
gptkb:battle
|
|
gptkbp:elevation
|
7.8 km/s
|
|
gptkbp:engine
|
gptkb:RD-170
1 x RD-0120
|
|
gptkbp:engine_type
|
gptkb:rocket
|
|
gptkbp:events
|
100%
|
|
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_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
20,000 kg
heavy lift launch vehicle
1,500,000 kg
Energia family
|
|
gptkbp:launched
|
November 15, 1987
limited to 1987-1988
|
|
gptkbp:manufacturer
|
gptkb:Monarch
|
|
gptkbp:market
|
estimated $170 million
|
|
gptkbp:mission
|
gptkb:Buran
|
|
gptkbp:notable_features
|
high payload capacity
|
|
gptkbp:number_of_stages
|
1 x RD-0120
4 x RD-170
|
|
gptkbp:operational_area
|
1987-1988
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:production_location
|
gptkb:Russia
|
|
gptkbp:propulsion
|
RP-1 and Liquid Oxygen
|
|
gptkbp:related_to
|
gptkb:spacecraft
|
|
gptkbp:seating_capacity
|
100,000 kg
5.5 m diameter
satellites, space probes
|
|
gptkbp:status
|
retired
|
|
gptkbp:strategic_importance
|
gptkb:0
|
|
gptkbp:succeeded_by
|
2
|
|
gptkbp:successor
|
gptkb:Angara_rocket
|
|
gptkbp:technology
|
liquid-fueled rocket
|
|
gptkbp:used_in
|
gptkb:Buran_program
|