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gptkbp:instance_of
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gptkb:Soyuz_spacecraft
gptkb:space_mission
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|
gptkbp:collaboration
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gptkb:JAXA
gptkb:ESA
gptkb:NASA
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gptkbp:communication_system
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S-band and Ku-band
Solar panels and batteries
|
|
gptkbp:cooling_system
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Reinforced carbon-carbon
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|
gptkbp:crew
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gptkb:Commander
gptkb:civil_aviation
gptkb:Japanese
gptkb:Oleg_Artemyev
gptkb:Soyuz_MS_descent_module
gptkb:Oleg_Novitskiy
gptkb:Star_City,_Russia
gptkb:Koichi_Wakata
gptkb:Mark_T._Vande_Hei
gptkb:Soyuz_MS
gptkb:Denis_Matveev
gptkb:Soyuz_MS_launch_vehicle
gptkb:Raja_Chari
gptkb:American
gptkb:Russian
gptkb:launch_escape_system
gptkb:missions
6 months
Indian
2023-09-30
extensive training
2023-03-30
experienced astronauts
Telemetry system
10:00 UTC
03:55 UTC
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:crew_launch_status
|
launched successfully
|
|
gptkbp:crew_return_status
|
landed safely
|
|
gptkbp:crew_training_simulator
|
Soyuz simulator
|
|
gptkbp:date
|
2023-09-30
|
|
gptkbp:debut
|
gptkb:2023
|
|
gptkbp:duration
|
approximately 6 months
|
|
gptkbp:first_flight
|
2023-09-30
2023-03-30
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz MS-53
|
|
gptkbp:is_a_destination_for
|
gptkb:International_Space_Station
|
|
gptkbp:landing_site
|
gptkb:Kazakhstan
|
|
gptkbp:launch_date
|
2023-03-30
03:55 UTC
|
|
gptkbp:launch_event
|
Successful
|
|
gptkbp:launch_mass
|
7,200 kg
|
|
gptkbp:launch_platform
|
gptkb:Arianespace
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz-2.1a
gptkb:Soyuz_2.1b
|
|
gptkbp:life_support_system
|
Closed-loop system
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mission
|
gptkb:Ts_UP-Moscow
gptkb:Scientific_research
gptkb:2023
gptkb:Soyuz_MS-52
gptkb:Soyuz_MS-53_patch
Completed
2023-09-30
completed
successful
Technology demonstration
Flight controllers
10:00 UTC
ISS crew rotation
transport crew to ISS
Soyuz MS-53 mission patch
|
|
gptkbp:mission_duration
|
180
approximately 6 months
180 days
approximately 180 days
|
|
gptkbp:mission_type
|
crewed
Crewed mission
|
|
gptkbp:navigation_system
|
Inertial navigation system
|
|
gptkbp:notable_mission
|
part of ISS program
|
|
gptkbp:operator
|
gptkb:Russian_space_agency
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:payload_capacity
|
2.2 m
2.7 m
2,500 kg
7.2 m
3.4 m
7,200 kg
|
|
gptkbp:preceded_by
|
gptkb:Soyuz_MS-52
|
|
gptkbp:predecessor
|
gptkb:Soyuz_MS-52
|
|
gptkbp:primary_mission
|
gptkb:Soyuz_MS-54
|
|
gptkbp:propulsion
|
Hypergolic propellants
|
|
gptkbp:recovery_method
|
Parachute system
|
|
gptkbp:related_vehicle
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:spacecraft
|
gptkb:Soyuz_MS_series
gptkb:Soyuz_MS-53
gptkb:Soyuz_MS
Crewed spacecraft
|
|
gptkbp:speed
|
28,000 km/h
|
|
gptkbp:succeeded_by
|
gptkb:Soyuz_MS-54
|
|
gptkbp:successor
|
gptkb:Soyuz_MS-54
|
|
gptkbp:sustainability
|
25 m²
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_spacecraft
gptkb:Peggy_Whitson
gptkb:Expedition_45
|
|
gptkbp:bfsLayer
|
4
|