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gptkbp:instance_of
|
gptkb:spacecraft
gptkb:Soyuz_spacecraft
gptkb:space_mission
|
|
gptkbp:air_traffic_control
|
digital
|
|
gptkbp:aircraft_operated
|
approximately 180 days
|
|
gptkbp:collaboration
|
gptkb:JAXA
gptkb:ESA
gptkb:Roscosmos
gptkb:CSA
gptkb:NASA
NASA, ESA, Roscosmos
|
|
gptkbp:communication_system
|
yes
solar panels
S-band and Ku-band
|
|
gptkbp:cooling_system
|
yes
ablative heat shield
|
|
gptkbp:crew
|
gptkb:Commander
gptkb:civil_aviation
gptkb:Luca_Parmitano
gptkb:Soyuz_MS-42
gptkb:Gagarin_Cosmonaut_Training_Center
gptkb:Samantha_Cristoforetti
gptkb:Oleg_Kononenko
gptkb:Soyuz_MS-42_descent_module
gptkb:3
gptkb:Kazakhstan
gptkb:Soyuz_MS_descent_module
gptkb:Alexander_Gerst
gptkb:Oleg_Novitskiy
gptkb:Mark_T._Vande_Hei
gptkb:Soyuz_2.1a
gptkb:Star_City
gptkb:Launch_Escape_System_(LES)
gptkb:launch_escape_system
gptkb:missions
6 months
yes
international
simulator training
2023-09-01
extensive
2023-03-01
mandatory
survival training
language training
extensive training
physical fitness training
Various space missions
Kononenko, Parmitano, Cristoforetti
Soyuz MS-42 capsule
NASA health protocols
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:crew_communication_system
|
S-band radio
|
|
gptkbp:crew_emergency_procedures
|
Standard operating procedures
|
|
gptkbp:data_return
|
2023-09-01 to 2023-09-10
|
|
gptkbp:date
|
2023-09-01
|
|
gptkbp:docking_system
|
gptkb:APAS
|
|
gptkbp:duration
|
approximately 6 months
|
|
gptkbp:emergency_services
|
yes
|
|
gptkbp:first_flight
|
gptkb:42
2023-09-01
2023-03-01
2016-11-17
|
|
gptkbp:height
|
3.4 m
|
|
gptkbp:historical_significance
|
part of ISS program
part of long-duration ISS missions.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz MS-42
|
|
gptkbp:is_a_destination_for
|
gptkb:International_Space_Station
|
|
gptkbp:landing_distance
|
gptkb:parachute
Soft landing system
|
|
gptkbp:landing_site
|
gptkb:Kazakhstan
|
|
gptkbp:launch_date
|
2023-03-01
12:00 UTC
03:55 UTC
|
|
gptkbp:launch_event
|
gptkb:true
successful
|
|
gptkbp:launch_mass
|
7,200 kg
|
|
gptkbp:launch_operator
|
gptkb:Roscosmos
|
|
gptkbp:launch_platform
|
gptkb:Arianespace
gptkb:Baikonur
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz-2.1b
gptkb:Soyuz_2.1a
|
|
gptkbp:launch_window
|
2023-03-01 to 2023-03-10
|
|
gptkbp:launched
|
gptkb:Russian_space_agency
Site 31/6
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:life_support_system
|
gptkb:Environmental_Control_and_Life_Support_System_(ECLSS)
yes
closed-loop system
|
|
gptkbp:manufacturer
|
gptkb:Russian_space_agency
gptkb:RSC_Energia
|
|
gptkbp:mass
|
2,500 kg
7,200 kg
|
|
gptkbp:mission
|
gptkb:Moscow
gptkb:Moscow_Mission_Control_Center
gptkb:Soyuz_MS-43
gptkb:Soyuz_MS-42_patch
gptkb:Soyuz_MS-41
gptkb:Expedition_68
gptkb:scientific_research
Completed
yes
completed
crew rotation
Transport crew to ISS
transport crew to ISS
ISS resupply
Soyuz MS-42 mission patch
|
|
gptkbp:mission_duration
|
6 months
approximately 6 months
approximately 180 days
|
|
gptkbp:mission_type
|
Crewed
crewed
|
|
gptkbp:module
|
2,500 kg
|
|
gptkbp:navigation_system
|
yes
inertial navigation
|
|
gptkbp:operational_since
|
gptkb:2023
|
|
gptkbp:operator
|
gptkb:Russian_space_agency
|
|
gptkbp:orbit_type
|
VHF radio system
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:orbital_period
|
90 minutes
|
|
gptkbp:part_of
|
gptkb:Soyuz_program
|
|
gptkbp:payload_capacity
|
2.7 m
up to 500 kg
7.2 m
3.4 m
7,200 kg
10 m³
|
|
gptkbp:predecessor
|
gptkb:Soyuz_MS-41
|
|
gptkbp:primary_mission
|
gptkb:Soyuz_MS-43
|
|
gptkbp:propulsion
|
Hypergolic propellant
hypergolic
|
|
gptkbp:recovery_method
|
gptkb:Kazakhstan
soft landing
|
|
gptkbp:related_vehicle
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:research
|
Material science
Biological studies
Microgravity research
Technology demonstrations
|
|
gptkbp:safety_features
|
redundant systems
multiple redundancy
|
|
gptkbp:service
|
gptkb:Soyuz_MS_service_module
3,000 kg
Soyuz MS-42 service module
|
|
gptkbp:spacecraft
|
gptkb:Soyuz_MS-42
gptkb:Soyuz_MS
Parachute recovery system
Three-module design
three-module design
1,000 W
|
|
gptkbp:spacecraft_mission_profile
|
Low Earth orbit mission
|
|
gptkbp:spacecraft_navigation
|
Inertial navigation system
|
|
gptkbp:spacecraft_reentry
|
Controlled reentry
|
|
gptkbp:spacecraft_thermal_control
|
Passive thermal control system
|
|
gptkbp:speed
|
2023-09-01
28,000 km/h
ballistic
|
|
gptkbp:status
|
active
|
|
gptkbp:successor
|
gptkb:Soyuz_MS-43
|
|
gptkbp:type
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:width
|
2.2 m
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_spacecraft
gptkb:Peggy_Whitson
gptkb:Expedition_45
|
|
gptkbp:bfsLayer
|
4
|