|
gptkbp:instance_of
|
gptkb:spacecraft
gptkb:Soyuz_spacecraft
gptkb:space_mission
|
|
gptkbp:collaboration
|
gptkb:JAXA
gptkb:ESA
gptkb:NASA
|
|
gptkbp:communication_system
|
S-band and Ku-band
|
|
gptkbp:cooling_system
|
active thermal control system
|
|
gptkbp:crew
|
gptkb:Commander
gptkb:civil_aviation
gptkb:Gagarin_Cosmonaut_Training_Center
gptkb:Samantha_Cristoforetti
gptkb:Oleg_Kononenko
gptkb:Soyuz-2.1b_launch_vehicle
gptkb:Soyuz_MS_descent_module
gptkb:Soyuz_MS_crew_return_vehicle
gptkb:Alexander_Gerst
gptkb:Oleg_Novitskiy
gptkb:Mark_T._Vande_Hei
gptkb:launch_escape_system
gptkb:missions
2023-09-15
simulator training
survival training
technical training
language training
2024-03-15
physical fitness training
extensive training program
biomedical monitoring system
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:date
|
2023-09-30
2024-03-15
|
|
gptkbp:docking_system
|
probe and drogue docking system
|
|
gptkbp:duration
|
6 months
approximately 6 months
|
|
gptkbp:first_flight
|
gptkb:2023
83
2023-09-15
2024-03-15
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz MS-83
|
|
gptkbp:is_a_destination_for
|
gptkb:International_Space_Station
|
|
gptkbp:landing_site
|
gptkb:Kazakhstan
|
|
gptkbp:launch_date
|
2023-09-15
2023-03-30
12:00 UTC
11:00 UTC
03:00 UTC
|
|
gptkbp:launch_event
|
successful
|
|
gptkbp:launch_mass
|
7,200 kg
14,000 kg
|
|
gptkbp:launch_platform
|
gptkb:Arianespace
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
Site 31/6
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz-2.1b
gptkb:Soyuz_2.1b
|
|
gptkbp:launch_window
|
September 2023
|
|
gptkbp:launched
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:life_support_system
|
closed-loop system
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mission
|
gptkb:Soyuz_MS-84
gptkb:Moscow
gptkb:Soyuz_MS-82
gptkb:scientific_research
completed
international cooperation
technology demonstration
transport crew to ISS
support ISS operations
Soyuz MS-83 patch
Soyuz MS-83 mission patch
|
|
gptkbp:mission_duration
|
approximately 6 months
approximately 180 days
|
|
gptkbp:mission_type
|
crewed
crewed mission
|
|
gptkbp:module
|
gptkb:Soyuz_MS_descent_module
|
|
gptkbp:navigation_system
|
gptkb:navigation_system
|
|
gptkbp:number_of_stages
|
gptkb:RD-0110_engine
gptkb:RD-107_A_engines
gptkb:RD-108_A_engines
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:operator
|
gptkb:Russian_space_agency
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:orbital_period
|
approximately 90 minutes
|
|
gptkbp:part_of
|
gptkb:Soyuz_program
|
|
gptkbp:payload_capacity
|
2.7 m
7.2 m
3.4 m
7,200 kg
7.2 m length
up to 500 kg to ISS
|
|
gptkbp:predecessor
|
gptkb:Soyuz_MS-82
|
|
gptkbp:primary_mission
|
gptkb:Soyuz_MS-84
|
|
gptkbp:recovery_area
|
gptkb:Kazakhstan
|
|
gptkbp:related_vehicle
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:research
|
gptkb:technology_demonstrations
gptkb:Earth_observation
materials science
microgravity research
biological studies
|
|
gptkbp:service
|
gptkb:Soyuz_MS_service_module
|
|
gptkbp:spacecraft
|
gptkb:spacecraft
gptkb:Soyuz_MS
modular design
|
|
gptkbp:speed
|
ballistic reentry
|
|
gptkbp:successor
|
gptkb:Soyuz_MS-84
|
|
gptkbp:support
|
up to 30 days
|
|
gptkbp:sustainability
|
two solar arrays
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_spacecraft
gptkb:Peggy_Whitson
gptkb:Expedition_45
|
|
gptkbp:bfsLayer
|
4
|