gptkbp:instance_of
|
gptkb:Soyuz_spacecraft
gptkb:space_mission
|
gptkbp:air_traffic_control
|
gptkb:Moscow_Mission_Control_Center
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gptkbp:collaboration
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gptkb:ESA
gptkb:Roscosmos
gptkb:NASA
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gptkbp:communication_system
|
S-band and Ku-band
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gptkbp:cooling_system
|
ablative heat shield
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gptkbp:crew
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gptkb:Commander
gptkb:civil_aviation
gptkb:Gagarin_Cosmonaut_Training_Center
gptkb:Samantha_Cristoforetti
gptkb:Sergei_Kud-Sverchkov
gptkb:Baikonur_Cosmodrome
gptkb:Kazakhstan
gptkb:Dmitry_Petelin
gptkb:Alexander_Gerst
gptkb:Oleg_Novitskiy
gptkb:Mark_T._Vande_Hei
gptkb:Andrey_Babkin
gptkb:Star_City
2023-09-15
ongoing
2024-03-15
mission specialist
parachute landing
ground control team
conducted pre-launch
pre-launch training
pre-launch and post-landing
radio and video links
|
gptkbp:crew_capacity
|
gptkb:3
|
gptkbp:crew_launch_method
|
gptkb:Team_Rocket
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gptkbp:date
|
2024-03-15
|
gptkbp:debut
|
gptkb:2023
|
gptkbp:duration
|
approximately 6 months
|
gptkbp:first_flight
|
gptkb:2023
2024
|
gptkbp:historical_significance
|
part of long-term ISS missions
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz MS-90
|
gptkbp:is_a_destination_for
|
gptkb:International_Space_Station
|
gptkbp:landing_site
|
gptkb:Kazakhstan
|
gptkbp:launch_date
|
2023-09-15
12:00 UTC
11:00 UTC
2023-09-15 T12:00:00 Z
|
gptkbp:launch_event
|
successful
|
gptkbp:launch_mass
|
9,500 kg
|
gptkbp:launch_platform
|
gptkb:Russian_space_agency
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
gptkbp:launch_vehicle
|
gptkb:Soyuz_2.1b
|
gptkbp:launch_window
|
September 2023
|
gptkbp:launched
|
approximately 10 hours
|
gptkbp:life_support_system
|
closed-loop system
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
gptkbp:mission
|
gptkb:Russian_Federal_Space_Agency
gptkb:Moscow
gptkb:Soyuz_MS-89
gptkb:Soyuz_MS-91
gptkb:scientific_research
data collection
completed
ISS crew rotation
designed by crew
Soyuz MS-90 mission patch
|
gptkbp:mission_duration
|
approximately 180 days
|
gptkbp:mission_type
|
crewed
crewed mission
|
gptkbp:operational_status
|
active
|
gptkbp:operator
|
gptkb:Russian_space_agency
|
gptkbp:orbit_type
|
low Earth orbit
|
gptkbp:orbital_altitude
|
400 km
|
gptkbp:orbital_inclination
|
51.6 degrees
|
gptkbp:payload_capacity
|
2.2 m
7.2 m
3.4 m
up to 3,000 kg
7,200 kg
|
gptkbp:power_source
|
solar panels
|
gptkbp:primary_mission
|
gptkb:Soyuz_MS-91
|
gptkbp:related_vehicle
|
gptkb:Soyuz_descent_module
gptkb:Soyuz_spacecraft
gptkb:Soyuz_MS_descent_module
|
gptkbp:research
|
various microgravity studies
|
gptkbp:safety_features
|
gptkb:launch_escape_system
|
gptkbp:spacecraft
|
gptkb:Soyuz_MS-90
gptkb:Soyuz_MS
three-module design
|
gptkbp:speed
|
gptkb:shield
|
gptkbp:successor
|
gptkb:Soyuz_MS-91
|
gptkbp:support
|
180 days
|
gptkbp:team
|
Russian recovery forces
|
gptkbp:bfsParent
|
gptkb:Soyuz_spacecraft
gptkb:Peggy_Whitson
gptkb:Expedition_45
|
gptkbp:bfsLayer
|
4
|