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gptkbp:instance_of
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gptkb:spacecraft
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gptkbp:collaboration
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gptkb:Intercosmos_program
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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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digital
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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:Gagarin_Cosmonaut_Training_Center
gptkb:Soyuz_30
gptkb:Soyuz_36
gptkb:launch_escape_system
safely returned
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gptkbp:crew_capacity
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gptkb:3
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gptkbp:designed_by
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gptkb:Soviet_Union
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gptkbp:diameter
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2.2 m
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gptkbp:docking_system
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probe and drogue
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gptkbp:first_flight
|
1979-03-28
1986-02-05
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gptkbp:flight_style
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gptkb:6
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gptkbp:historical_significance
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first spacecraft to use digital control systems.
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|
https://www.w3.org/2000/01/rdf-schema#label
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Soyuz-T
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gptkbp:landing_site
|
1986-02-05
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gptkbp:launch_date
|
1979-03-28
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gptkbp:launch_mass
|
6800 kg
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gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
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gptkbp:launch_vehicle
|
gptkb:Soyuz_spacecraft
|
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gptkbp:launched
|
gptkb:6
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|
gptkbp:length
|
7.2 m
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gptkbp:life_support_system
|
closed-loop
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gptkbp:manufacturer
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gptkb:Yuzhnoye_Design_Office
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gptkbp:mission
|
gptkb:6
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gptkbp:mission_duration
|
up to 180 days
|
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gptkbp:mission_type
|
low Earth orbit
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gptkbp:module
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gptkb:Soyuz_spacecraft
|
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gptkbp:navigation_system
|
inertial navigation
|
|
gptkbp:notable_mission
|
gptkb:Soyuz_30
gptkb:Soyuz_36
|
|
gptkbp:operational_period
|
1979-1986
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gptkbp:orbital_period
|
90 minutes
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gptkbp:payload_capacity
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up to 1000 kg
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gptkbp:power_source
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solar panels
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gptkbp:recovery_method
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gptkb:parachute
|
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gptkbp:replaced_by
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gptkb:Soyuz_TM
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gptkbp:safety_record
|
high safety record
|
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gptkbp:service
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gptkb:Public_service
|
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gptkbp:spacecraft
|
gptkb:spacecraft
|
|
gptkbp:speed
|
descent capsule
|
|
gptkbp:status
|
retired
|
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gptkbp:successor
|
gptkb:Soyuz_TM
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gptkbp:used_for
|
manned spaceflight
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gptkbp:bfsParent
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gptkb:Soyuz_T-26
gptkb:Soyuz_T-45
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gptkbp:bfsLayer
|
5
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