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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:navigation_system
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gptkbp:collaboration
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yes
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gptkbp:communication_system
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gptkb:radio_station
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gptkbp:control_system
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automatic and manual
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gptkbp:cooling_system
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yes
ablative heat shield
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gptkbp:crew
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gptkb:Valery_Ryumin
gptkb:3
gptkb:Viktor_Savinykh
gptkb:Valentina_Tereshkova
gptkb:Alexander_Serebrov
gptkb:launch_escape_system
yes
Cosmonaut training program
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gptkbp:crew_capacity
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gptkb:3
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gptkbp:decommissioned
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gptkb:1981
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gptkbp:descent_mass
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2,500 kg
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gptkbp:design
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3 years
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gptkbp:design_purpose
|
transport to space stations
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gptkbp:diameter
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2.2 m
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gptkbp:first_flight
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gptkb:1976
gptkb:1980
gptkb:1981
gptkb:1983
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gptkbp:flight_style
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gptkb:10
gptkb:3
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gptkbp:height
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3.2 m
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gptkbp:historical_significance
|
part of the Soviet space program
contributed to long-duration spaceflight research
first spacecraft to dock with Salyut 7
first spacecraft to support long-duration missions.
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|
https://www.w3.org/2000/01/rdf-schema#label
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Soyuz 85 K
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gptkbp:influenced
|
future spacecraft designs
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gptkbp:influenced_by
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gptkb:Soyuz_7_K_series
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gptkbp:is_aplace_for
|
400 km
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gptkbp:landing_distance
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gptkb:parachute
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|
gptkbp:landing_site
|
1981-02-10
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gptkbp:launch_date
|
1976-11-10
1980-11-20
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gptkbp:launch_mass
|
7,200 kg
|
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gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz_spacecraft
gptkb:Team_Rocket
|
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gptkbp:launched
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gptkb:10
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gptkbp:length
|
7.2 m
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gptkbp:life_support_system
|
yes
closed-loop system
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gptkbp:manufacturer
|
gptkb:Soviet_Union
|
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gptkbp:mass
|
7,200 kg
|
|
gptkbp:mission
|
gptkb:Moscow_Mission_Control_Center
|
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gptkbp:mission_duration
|
90 days
up to 30 days
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gptkbp:mission_type
|
gptkb:scientific_research
manned
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gptkbp:navigation_system
|
inertial navigation
|
|
gptkbp:notable_mission
|
gptkb:Mir
gptkb:Salyut_7
gptkb:International_Space_Station
|
|
gptkbp:operational_period
|
1976-1981
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gptkbp:operational_status
|
retired
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gptkbp:operational_use
|
manned missions to Salyut stations
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|
gptkbp:orbital_altitude
|
yes
200-400 km
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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
up to 1,000 kg
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|
gptkbp:perigee
|
200 km
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|
gptkbp:power_source
|
solar panels
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gptkbp:predecessor
|
gptkb:Soyuz_7_K
|
|
gptkbp:purpose
|
manned spaceflight
|
|
gptkbp:recovery_method
|
gptkb:parachute
parachute recovery
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|
gptkbp:related_vehicle
|
gptkb:Soyuz_descent_module
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:service
|
gptkb:Soyuz_service_module
yes
|
|
gptkbp:significant_event
|
first flight in 1976
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|
gptkbp:spacecraft
|
gptkb:spacecraft
three-module design
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|
gptkbp:speed
|
yes
28,000 km/h
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gptkbp:successor
|
gptkb:Soyuz_T
|
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gptkbp:weight
|
7,200 kg
|
|
gptkbp:width
|
2.2 m
|