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gptkbp:instance_of
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gptkb:spacecraft
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gptkbp:air_traffic_control
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gptkb:Racing
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gptkbp:collaboration
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Soviet Union and international partners
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|
gptkbp:communication
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gptkb:radio_station
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gptkbp:control_system
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gptkb:navigation_system
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|
gptkbp:cooling_system
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ablative heat shield
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gptkbp:crew
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gptkb:Soyuz_35
gptkb:Soyuz_36
gptkb:launch_escape_system
2
extensive
biomedical sensors
|
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gptkbp:crew_capacity
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gptkb:3
|
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gptkbp:diameter
|
2.7 meters
|
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gptkbp:emergency_services
|
detailed protocols
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gptkbp:first_flight
|
gptkb:Soyuz_7_K-T_No._52_K
1980-11-20
1981-04-05
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gptkbp:flight_style
|
2
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gptkbp:height
|
7.3 meters
|
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gptkbp:historical_significance
|
first flight after redesign
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz 52 K
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gptkbp:is_a_destination_for
|
gptkb:Salyut_7
|
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gptkbp:launch_date
|
1980-11-20
1987-12-21
|
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gptkbp:launch_mass
|
7,200 kg
|
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gptkbp:launch_platform
|
gptkb:ground
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz-U
|
|
gptkbp:launch_window
|
2 minutes
|
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gptkbp:launched
|
2
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gptkbp:legacy
|
foundation for future Soyuz missions
|
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gptkbp:life_support_system
|
closed-loop system
|
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gptkbp:manufacturer
|
gptkb:Soyuz_Design_Bureau
|
|
gptkbp:mass
|
7,200 kg
|
|
gptkbp:mission
|
successful
|
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gptkbp:mission_duration
|
7 days
|
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gptkbp:mission_type
|
gptkb:human_spaceflight
crewed
|
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gptkbp:module
|
gptkb:Soyuz_descent_module
|
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gptkbp:navigation_system
|
star tracker
|
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gptkbp:operational_period
|
1980-1981
|
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gptkbp:orbital_inclination
|
51.6 degrees
|
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gptkbp:orbital_period
|
90 minutes
|
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gptkbp:payload_capacity
|
1,000 kg
|
|
gptkbp:power_source
|
solar panels
|
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gptkbp:propulsion
|
hypergolic propellants
|
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gptkbp:recovery_method
|
gptkb:parachute
gptkb:Kazakhstan
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:service
|
gptkb:Soyuz_service_module
|
|
gptkbp:speed
|
28,000 km/h
|
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gptkbp:status
|
retired
|
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gptkbp:successor
|
gptkb:Soyuz_T
|