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gptkbp:instance_of
|
gptkb:Space_Shuttle
|
|
gptkbp:air_traffic_control
|
autonomous landing system
|
|
gptkbp:aircraft_operated
|
3 hours 25 minutes
|
|
gptkbp:cancellation_reason
|
political and economic factors
|
|
gptkbp:cargo_capacity
|
30,000 kg
100 m³
|
|
gptkbp:conducts_research_on
|
microgravity experiments
|
|
gptkbp:control_system
|
digital fly-by-wire
|
|
gptkbp:cooling_system
|
reinforced carbon-carbon
|
|
gptkbp:country
|
gptkb:Soviet_Union
|
|
gptkbp:crew
|
yes
|
|
gptkbp:crew_capacity
|
gptkb:5
|
|
gptkbp:design
|
gptkb:Vladimir_Chelomey
similar to Space Shuttle
|
|
gptkbp:design_features
|
delta wing configuration
|
|
gptkbp:design_purpose
|
orbital spaceflight
|
|
gptkbp:design_team_leader
|
gptkb:Vladimir_Chelomey
|
|
gptkbp:designed_for
|
gptkb:human_spaceflight
|
|
gptkbp:developed_by
|
gptkb:Soviet_Union
|
|
gptkbp:development
|
gptkb:1976
gptkb:1988
|
|
gptkbp:durability
|
gptkb:true
|
|
gptkbp:duration
|
12 years
|
|
gptkbp:emergency_services
|
1993 hangar collapse
|
|
gptkbp:engine
|
gptkb:4
|
|
gptkbp:engine_type
|
gptkb:RD-0120
|
|
gptkbp:fate
|
destroyed in hangar collapse
|
|
gptkbp:first_flight
|
successful
15 November 1988
|
|
gptkbp:flight_style
|
gptkb:1
|
|
gptkbp:has_programs
|
gptkb:Buran_program
cancelled
|
|
gptkbp:height
|
16.4 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Buran space shuttle
|
|
gptkbp:inaugural_flight_duration
|
3 hours 25 minutes
|
|
gptkbp:influence
|
inspired future spacecraft designs
|
|
gptkbp:influenced_by
|
gptkb:Apollo_program
|
|
gptkbp:inspiration
|
gptkb:NASA_Space_Shuttle
|
|
gptkbp:involved_in
|
international space collaboration
|
|
gptkbp:is_influenced_by
|
spaceplane technology
|
|
gptkbp:landing_distance
|
autonomous
220 km/h
80,000 kg
|
|
gptkbp:landing_site
|
15 November 1988
|
|
gptkbp:launch_date
|
15 November 1988
|
|
gptkbp:launch_mass
|
200,000 kg
105,000 kg
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Energia
gptkb:Energia_rocket
|
|
gptkbp:legacy
|
remains a symbol of Soviet space achievements
|
|
gptkbp:length
|
37.5 meters
|
|
gptkbp:manufacturer
|
gptkb:OKB-1
|
|
gptkbp:max_takeoff_weight
|
105,000 kg
|
|
gptkbp:notable_feature
|
automated landing system
|
|
gptkbp:notable_mission
|
successful unmanned flight
|
|
gptkbp:notable_technology
|
orbital maneuvering system
|
|
gptkbp:number_of_engines
|
gptkb:4
|
|
gptkbp:operated_by
|
gptkb:Russian_Federal_Space_Agency
|
|
gptkbp:operational_cost
|
estimated $170 million per flight
|
|
gptkbp:operational_period
|
1988-1993
|
|
gptkbp:orbital_altitude
|
100 km
6,000 km
performed
28,000 km/h
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:orbital_payload
|
30,000 kg
|
|
gptkbp:orbital_period
|
up to 10 days
|
|
gptkbp:payload_bay_height
|
3.7 meters
|
|
gptkbp:payload_bay_length
|
18.5 meters
|
|
gptkbp:payload_bay_width
|
4.6 meters
|
|
gptkbp:payload_capacity
|
30,000 kg
|
|
gptkbp:primary_use
|
gptkb:scientific_research
|
|
gptkbp:recovery_method
|
landing on runway
|
|
gptkbp:related_to
|
gptkb:Soviet_space_program
|
|
gptkbp:release_date
|
gptkb:1984
|
|
gptkbp:retirement
|
end of the Soviet Union
|
|
gptkbp:significance
|
first fully automated space shuttle flight
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:none
gptkb:Energia
|
|
gptkbp:twin_engines
|
2
|
|
gptkbp:used_for
|
satellite deployment
|
|
gptkbp:weight
|
100,000 kg
105,000 kg
|
|
gptkbp:wingspan
|
24 meters
|