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gptkbp:instance_of
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gptkb:spacecraft
|
|
gptkbp:collaboration
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gptkb:Mir_program
gptkb:NASA_and_ESA
gptkb:ESA
gptkb:Roscosmos
gptkb:NASA
ESA, NASA
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|
gptkbp:communication_system
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gptkb:radio_station
|
|
gptkbp:control_system
|
fly-by-wire
digital flight control system
|
|
gptkbp:cooling_system
|
phenolic resin
ablative heat shield
|
|
gptkbp:crew
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gptkb:Gagarin_Cosmonaut_Training_Center
gptkb:Valery_Polyakov
gptkb:Star_City
gptkb:launch_escape_system
cosmonauts and astronauts
reclined seats
NASA and Roscosmos
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:decommissioned
|
gptkb:2002
gptkb:2009
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|
gptkbp:design_features
|
modular design
|
|
gptkbp:designed_by
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gptkb:Soviet_Union
|
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gptkbp:diameter
|
2.2 m
|
|
gptkbp:docking_system
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gptkb:Mir_space_station
gptkb:International_Space_Station
gptkb:APAS
|
|
gptkbp:emergency_services
|
predefined protocols
|
|
gptkbp:first_flight
|
gptkb:Soyuz_TM-12
gptkb:1986
gptkb:2001
gptkb:Soyuz_TM-1
1986-12-20
2009-04-08
2002-04-25
1986-03-20
|
|
gptkbp:first_manned_mission
|
gptkb:Soyuz_TM-1
|
|
gptkbp:flight_style
|
gptkb:12
gptkb:15
|
|
gptkbp:historical_significance
|
first spacecraft to dock with Mir
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz TM
|
|
gptkbp:influenced
|
future spacecraft designs
|
|
gptkbp:influenced_by
|
gptkb:Soyuz_program
|
|
gptkbp:inspiration
|
modern spacecraft designs
|
|
gptkbp:landing_site
|
gptkb:Kazakhstan
|
|
gptkbp:last_manned_mission
|
gptkb:Soyuz_TM-34
|
|
gptkbp:launch_date
|
gptkb:1986
annual
1986-12-20
|
|
gptkbp:launch_mass
|
7,200 kg
|
|
gptkbp:launch_price
|
$30 million
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz-U
gptkb:Soyuz_spacecraft
|
|
gptkbp:legacy
|
foundation for future Soyuz models
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:life_support_system
|
closed-loop system
|
|
gptkbp:manufacturer
|
gptkb:Soyuz_Design_Bureau
gptkb:RSC_Energia
|
|
gptkbp:mission
|
gptkb:12
2001-04-16
|
|
gptkbp:mission_duration
|
up to 6 months
|
|
gptkbp:mission_type
|
gptkb:transportation
manned
crew transport
|
|
gptkbp:navigation_system
|
gptkb:navigation_system
inertial navigation
|
|
gptkbp:notable_mission
|
gptkb:Mir_space_station_missions
gptkb:Mir-1
|
|
gptkbp:operational_period
|
approximately 10 days
1986-2002
23 years
1986-2009
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:orbital_altitude
|
200-400 km
uses thrusters
|
|
gptkbp:orbital_period
|
90 minutes
|
|
gptkbp:payload_capacity
|
1,000 kg
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:primary_function
|
transport to space station
|
|
gptkbp:recovery_method
|
gptkb:parachute
|
|
gptkbp:related_vehicle
|
gptkb:Soyuz_descent_module
|
|
gptkbp:replaced_by
|
gptkb:Soyuz_TMA
|
|
gptkbp:safety_features
|
multiple redundancy
|
|
gptkbp:service
|
gptkb:Soyuz_service_module
provides propulsion
|
|
gptkbp:significant_event
|
first long-duration mission to Mir
|
|
gptkbp:speed
|
ballistic reentry
|
|
gptkbp:success_rate
|
100%
|
|
gptkbp:successor
|
gptkb:Soyuz_TMA_program
gptkb:Soyuz_TMA
gptkb:Soyuz_MS
|
|
gptkbp:training
|
6 months
|
|
gptkbp:type
|
gptkb:spacecraft
|
|
gptkbp:used_for
|
manned spaceflight
manned space missions
|
|
gptkbp:weight
|
7,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_96
gptkb:Soyuz_92
gptkb:Soyuz_TM-33
gptkb:Soyuz_47
gptkb:Soyuz_TM-18
gptkb:Soyuz_43
gptkb:Soyuz_T
gptkb:Soyuz_94
gptkb:Soyuz_TM-31
|
|
gptkbp:bfsLayer
|
5
|