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gptkbp:instance_of
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gptkb:spacecraft
gptkb:Soyuz_spacecraft
gptkb:space_mission
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gptkbp:air_traffic_control
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fly-by-wire system
Automated and manual control options
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|
gptkbp:aircraft_operated
|
Approximately 6 months
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|
gptkbp:collaboration
|
gptkb:JAXA
gptkb:ESA
gptkb:Roscosmos
gptkb:NASA
NASA, ESA, Roscosmos
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|
gptkbp:communication_system
|
S-band and Ku-band
Radio and telemetry
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gptkbp:control_system
|
Fly-by-wire system
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|
gptkbp:cooling_system
|
Heat shield
ablative heat shield
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|
gptkbp:crew
|
gptkb:Commander
gptkb:civil_aviation
gptkb:Gagarin_Cosmonaut_Training_Center
gptkb:Oleg_Kononenko
gptkb:Kazakhstan
gptkb:Soyuz_descent_module
gptkb:radio_station
gptkb:Alexander_Gerst
gptkb:Oleg_Novitskiy
gptkb:Star_City,_Russia
gptkb:Satoshi_Furukawa
gptkb:Mark_T._Vande_Hei
gptkb:American
gptkb:German
gptkb:Russian
gptkb:launch_escape_system
gptkb:missions
6 months
2024-03-15
emergency procedures training
pre-launch checks
Rigorous selection process
prior to launch
Cosmonaut training program
biomedical telemetry
post-landing checks
Designed for crew safety
Extensive training required
launch escape tower
based on experience
Experienced astronauts
via radio and video
monitored during mission
Continuous health monitoring during flight
pre-flight acclimatization
held before launch
ensured during flight
onboard Soyuz MS-96
provided by ground teams
Safe return of crew to Earth
post-landing recovery operations
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|
gptkbp:crew_capacity
|
gptkb:3
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|
gptkbp:crew_reintegration
|
after landing
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gptkbp:date
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2024-03-15
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|
gptkbp:debut
|
completed successfully
|
|
gptkbp:docking_system
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gptkb:APAS
|
|
gptkbp:duration
|
approximately 6 months
|
|
gptkbp:emergency_services
|
Established emergency protocols
ballistic descent
|
|
gptkbp:end_of_life
|
decommissioning process
|
|
gptkbp:first_flight
|
2023-09-15
2016-11-17
pre-flight testing
|
|
gptkbp:height
|
3.4 m
|
|
gptkbp:historical_significance
|
Part of long-term ISS missions
part of ISS program
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz MS-96
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|
gptkbp:is_a_destination_for
|
gptkb:International_Space_Station
|
|
gptkbp:landing_sequence
|
controlled descent
|
|
gptkbp:landing_site
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gptkb:Kazakhstan
|
|
gptkbp:launch_date
|
2023-09-15
12:00 UTC
11:00 UTC
14:00 UTC
|
|
gptkbp:launch_event
|
gptkb:true
Successful
High success rate
|
|
gptkbp:launch_mass
|
7,200 kg
|
|
gptkbp:launch_platform
|
gptkb:Baikonur_launch_control_center
gptkb:Arianespace
gptkb:Baikonur_launch_control
gptkb:Roscosmos
gptkb:Ground_control_at_Baikonur
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|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
Site 31/6
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|
gptkbp:launch_vehicle
|
gptkb:Soyuz-2.1b
gptkb:Soyuz_2.1b
|
|
gptkbp:launch_window
|
30 minutes
September 2023
2023-09-15 to 2023-09-30
|
|
gptkbp:launched
|
gptkb:Baikonur_Cosmodrome
T-10 minutes
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:life_support_system
|
Closed-loop system
closed-loop system
Closed-loop life support
|
|
gptkbp:manufacturer
|
gptkb:Russian_Federal_Space_Agency
gptkb:RSC_Energia
|
|
gptkbp:mass
|
3,000 kg
7,200 kg
|
|
gptkbp:mission
|
gptkb:Scientific_research
gptkb:Moscow_Mission_Control_Center
gptkb:Moscow_mission_control
gptkb:Soyuz_MS-95
gptkb:Expedition_70
International collaboration
completed
debriefing sessions
transport crew to ISS
Crew rotation
ISS resupply
Support ISS operations
recorded for future reference
conducted after return
Soyuz MS-96 patch
Conducted after each mission
Resupply ISS with cargo
|
|
gptkbp:mission_duration
|
6 months
approximately 6 months
180 days
detailed mission plan
|
|
gptkbp:mission_type
|
Crewed
crewed
crewed mission
|
|
gptkbp:module
|
2,500 kg
|
|
gptkbp:navigation_system
|
gptkb:navigation_system
Inertial navigation system
|
|
gptkbp:next_edition
|
gptkb:Soyuz_MS-97
|
|
gptkbp:operational_status
|
Operational
|
|
gptkbp:operator
|
gptkb:Russian_space_agency
|
|
gptkbp:orbit_type
|
successful
|
|
gptkbp:orbital_altitude
|
400 km
routine ISS operations
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:orbital_module_mass
|
2,200 kg
|
|
gptkbp:orbital_period
|
90 minutes
|
|
gptkbp:outcome
|
gptkb:true
|
|
gptkbp:part_of
|
gptkb:Soyuz_program
|
|
gptkbp:payload_capacity
|
up to 500 kg
7,200 kg
300 kg to ISS
|
|
gptkbp:power_source
|
Solar panels
solar panels
|
|
gptkbp:predecessor
|
gptkb:Soyuz_MS-95
|
|
gptkbp:previous_versions
|
gptkb:Soyuz_MS-95
|
|
gptkbp:primary_mission
|
gptkb:Soyuz_MS-97
|
|
gptkbp:recovery_method
|
Parachute landing
|
|
gptkbp:related_vehicle
|
gptkb:Soyuz_capsule
gptkb:Soyuz_spacecraft
|
|
gptkbp:research
|
conducted on ISS
Conducts various experiments on ISS
|
|
gptkbp:return_vehicle_separation
|
separation from ISS
|
|
gptkbp:safety_features
|
gptkb:launch_escape_system
|
|
gptkbp:safety_record
|
High safety record
|
|
gptkbp:service
|
2,500 kg
|
|
gptkbp:spacecraft
|
gptkb:Soyuz_MS
modular design
via helicopter
Three-module configuration
based on Soyuz TMA
tested pre-launch
Advanced avionics and systems
Multi-purpose spacecraft
|
|
gptkbp:speed
|
Heat shield
ballistic reentry
28,000 km/h
1.2 degrees
|
|
gptkbp:squadrons
|
White and blue
|
|
gptkbp:status
|
Active
|
|
gptkbp:successor
|
gptkb:Soyuz_MS-97
|
|
gptkbp:team
|
gptkb:Kazakhstan_Recovery_Forces
Russian recovery forces
|
|
gptkbp:training_programs
|
intensive preparation
|
|
gptkbp:weather_conditions
|
favorable conditions
|
|
gptkbp:width
|
2.7 m
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_spacecraft
gptkb:Peggy_Whitson
gptkb:Expedition_45
|
|
gptkbp:bfsLayer
|
4
|