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gptkbp:instanceOf
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space program
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gptkbp:collaborations
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gptkb:International_Space_Station
NASA,_ESA,_JAXA
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gptkbp:communicationEquipment
|
radio communication system
|
|
gptkbp:crew
|
gptkb:Gagarin_Cosmonaut_Training_Center
launch escape system
ISS crew rotation
biomedical monitoring
cosmonauts and astronauts
experienced astronauts and cosmonauts
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|
gptkbp:crew_size
|
3
international selection process
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gptkbp:dimensions
|
7.2 m length
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gptkbp:duration
|
approximately 6 months
|
|
gptkbp:electronic_systems
|
redundant systems
|
|
gptkbp:emergencyServices
|
well-defined emergency procedures
|
|
gptkbp:firstFlight
|
TMA-1
TMA-22
|
|
gptkbp:historical_significance
|
important for ISS operations
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz TMA program
|
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gptkbp:is_a_source_of
|
transport to ISS
|
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gptkbp:landing_gear
|
gptkb:Kazakhstan
|
|
gptkbp:launchDate
|
October 20, 2002
approximately 2-3 per year
September 21, 2011
|
|
gptkbp:launched
|
gptkb:Baikonur_launch_control_center
varies by mission
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz_rocket
orbital spacecraft
|
|
gptkbp:legacy
|
foundation for future crewed missions
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mission
|
crewed spaceflight
manned spacecraft
|
|
gptkbp:missions
|
gptkb:Moscow_Mission_Control_Center
22
TMA-11, TMA-12
|
|
gptkbp:navigationEquipment
|
inertial navigation system
|
|
gptkbp:notableWork
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:operates_in
|
gptkb:Russian_Federal_Space_Agency
|
|
gptkbp:operational_status
|
thorough post-mission analysis
|
|
gptkbp:operationalRange
|
approximately 400 km
|
|
gptkbp:partOf
|
gptkb:Soyuz_program
|
|
gptkbp:passenger_traffic
|
up to 100 kg
|
|
gptkbp:powerOutput
|
solar panels
|
|
gptkbp:productionYears
|
2002-2011
|
|
gptkbp:providesServices
|
closed-loop life support
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:renovated
|
parachute landing
|
|
gptkbp:replacedBy
|
gptkb:Soyuz_MS_program
|
|
gptkbp:research
|
microgravity research
|
|
gptkbp:returnPolicy
|
gptkb:Soyuz_descent_module
|
|
gptkbp:safetyFeatures
|
excellent safety record
|
|
gptkbp:secondary_mission
|
TMA-1
TMA-22
|
|
gptkbp:speed
|
28,000 km/h
|
|
gptkbp:successor
|
gptkb:Soyuz_MS_program
|
|
gptkbp:training
|
6 months
various training facilities
|
|
gptkbp:weight
|
7,200 kg
|