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gptkbp:instance_of
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gptkb:spacecraft
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gptkbp:collaboration
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gptkb:Russian_Federal_Space_Agency
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gptkbp:communication_system
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gptkb:radio_station
|
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gptkbp:crew
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gptkb:Commander
gptkb:engineers
gptkb:civil_aviation
gptkb:Soyuz_launch_vehicle
gptkb:Soyuz_descent_module
gptkb:Sergei_Avdeyev
gptkb:Star_City,_Russia
gptkb:Alexander_Balandin
gptkb:Viktor_Afanasyev
performed during mission
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|
gptkbp:crew_capacity
|
gptkb:3
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|
gptkbp:data_return
|
12:00 UTC
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|
gptkbp:end_of_life
|
decommissioned after mission.
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gptkbp:first_flight
|
gptkb:1998
gptkb:1999
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz TM-28
|
|
gptkbp:is_a_destination_for
|
gptkb:Mir_space_station
|
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gptkbp:landing_site
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gptkb:Kazakhstan
1999-01-21
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|
gptkbp:launch_date
|
1998-03-13
1998-07-22
12:38 UTC
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz-FG
|
|
gptkbp:life_support_system
|
closed-loop system
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mission
|
gptkb:Moscow_Mission_Control_Center
gptkb:Soyuz_TM-28_patch
completed
successful
crew rotation
conducted by RSC Energia
|
|
gptkbp:mission_duration
|
approximately 6 months
5 months, 10 days
|
|
gptkbp:mission_type
|
crewed mission
|
|
gptkbp:navigation_system
|
gptkb:navigation_system
|
|
gptkbp:operational_period
|
1998-1999
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:payload_capacity
|
7,200 kg
approximately 7,000 kg
|
|
gptkbp:recovery_method
|
gptkb:parachute
|
|
gptkbp:research
|
conducted during mission
|
|
gptkbp:significant_event
|
first flight of the new Soyuz spacecraft design
|
|
gptkbp:spacecraft
|
gptkb:Soyuz_TM_series
gptkb:Soyuz_TM
three-module design
|
|
gptkbp:speed
|
ballistic reentry
|
|
gptkbp:successor
|
gptkb:Soyuz_TM-29
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_95
gptkb:Gennady_Padalka
gptkb:Anatoli_Berezovoy
gptkb:Soyuz_99
gptkb:Soyuz_94
gptkb:Expedition_92
|
|
gptkbp:bfsLayer
|
5
|