|
gptkbp:instance_of
|
gptkb:spacecraft
gptkb:space_mission
|
|
gptkbp:air_traffic_control
|
digital flight control system
|
|
gptkbp:collaboration
|
NASA, JAXA, Roscosmos
|
|
gptkbp:communication_system
|
S-band and Ku-band
|
|
gptkbp:cooling_system
|
ablative heat shield
|
|
gptkbp:crew
|
gptkb:Gagarin_Cosmonaut_Training_Center
gptkb:Samantha_Cristoforetti
gptkb:Soyuz_descent_module
gptkb:radio_station
gptkb:Oleg_Novitskiy
gptkb:Koichi_Wakata
gptkb:Mark_T._Vande_Hei
gptkb:launch_escape_system
6 months
2024-03-15
pre-flight training
biomedical telemetry
varied spaceflight experience
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:crew_living_space
|
1.9 m³
|
|
gptkbp:date
|
2024-03-15
|
|
gptkbp:docking_system
|
gptkb:APAS_docking_system
|
|
gptkbp:duration
|
approximately 6 months
|
|
gptkbp:emergency_services
|
detailed emergency protocols
|
|
gptkbp:first_flight
|
2024-03-15
2016-11-17
|
|
gptkbp:historical_significance
|
part of ISS program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz MS-89
|
|
gptkbp:is_a_destination_for
|
gptkb:International_Space_Station
|
|
gptkbp:landing_distance
|
medical checks and debriefing
|
|
gptkbp:landing_site
|
gptkb:Kazakhstan
2024-03-15
|
|
gptkbp:launch_date
|
2023-09-15
|
|
gptkbp:launch_mass
|
7,200 kg
|
|
gptkbp:launch_platform
|
gptkb:Baikonur_launch_control
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz_2.1b
|
|
gptkbp:launch_window
|
2 hours
|
|
gptkbp:launched
|
approximately 10 hours
|
|
gptkbp:life_support_system
|
closed-loop system
|
|
gptkbp:manufacturer
|
gptkb:Russian_Federal_Space_Agency
|
|
gptkbp:mission
|
gptkb:Soyuz_MS-90
gptkb:Soyuz_MS-88
completed
ISS crew rotation
data collection and review
Soyuz MS-89 patch
|
|
gptkbp:mission_duration
|
approximately 6 months
approximately 180 days
|
|
gptkbp:mission_type
|
crewed
crewed mission
|
|
gptkbp:navigation_system
|
gptkb:navigation_system
|
|
gptkbp:operational_status
|
operational
|
|
gptkbp:operator
|
gptkb:Russian_space_agency
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:orbital_period
|
Low Earth Orbit
|
|
gptkbp:payload_capacity
|
2.2 m
7.2 m
3.4 m
up to 3,000 kg
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:propulsion
|
hypergolic thrusters
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:spacecraft
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:speed
|
7.5 km/s
|
|
gptkbp:squadrons
|
white and blue
|
|
gptkbp:successor
|
gptkb:Soyuz_MS-90
|
|
gptkbp:team
|
Kazakhstan recovery team
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_spacecraft
gptkb:Peggy_Whitson
gptkb:Expedition_45
|
|
gptkbp:bfsLayer
|
4
|