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gptkbp:instance_of
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gptkb:spacecraft
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|
gptkbp:cabin_access
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hatchway
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gptkbp:collaboration
|
NASA, ESA, JAXA
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|
gptkbp:communication_system
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gptkb:radio_station
|
|
gptkbp:control_surfaces
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canards
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gptkbp:control_system
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automatic and manual
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|
gptkbp:cooling_system
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phenolic resin
ablative heat shield
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|
gptkbp:crew
|
yes
required
several months
multiple redundancy systems
Alexey Gubarev, Valentina Tereshkova
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|
gptkbp:crew_capacity
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gptkb:3
3 seats in a row
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gptkbp:current_use
|
ISS crew transport
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gptkbp:debut
|
over 150 missions
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|
gptkbp:design
|
6 months
ongoing improvements
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gptkbp:design_features
|
conical shape
|
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gptkbp:designed_for
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gptkb:human_spaceflight
|
|
gptkbp:diameter
|
2.2 meters
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|
gptkbp:emergency_landing_options
|
land or water
|
|
gptkbp:emergency_services
|
yes
|
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gptkbp:first_flight
|
gptkb:Soyuz_MS-19
gptkb:1967
gptkb:Soyuz_1
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|
gptkbp:historical_significance
|
first spacecraft to carry humans to space and return safely
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz descent capsule
|
|
gptkbp:in-flight_monitoring
|
real-time telemetry
|
|
gptkbp:influenced_by
|
gptkb:Vostok_spacecraft
|
|
gptkbp:inspiration
|
other spacecraft designs
|
|
gptkbp:landing_distance
|
gptkb:parachute
|
|
gptkbp:launch_date
|
multiple per year
|
|
gptkbp:launch_platform
|
ground control team
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:length
|
2.5 meters
|
|
gptkbp:life_support_system
|
yes
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mass
|
7,200 kg
|
|
gptkbp:mission
|
debriefing sessions
|
|
gptkbp:mission_duration
|
Soyuz 7, Soyuz 11, Soyuz 18a
|
|
gptkbp:modifications
|
Soyuz T, Soyuz TM, Soyuz MS
|
|
gptkbp:module
|
approximately 3 hours
|
|
gptkbp:navigation_system
|
inertial navigation
|
|
gptkbp:notable_mission
|
gptkb:Apollo-Soyuz_Test_Project
|
|
gptkbp:number_of_rooms
|
approximately 5 cubic meters
|
|
gptkbp:operational_cost
|
relatively low
|
|
gptkbp:operational_since
|
gptkb:1967
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:origin
|
gptkb:Soviet_Union
|
|
gptkbp:parachute_deployment_altitude
|
10,000 feet
|
|
gptkbp:post_landing_procedure
|
crew extraction and medical checks
|
|
gptkbp:primary_function
|
cargo transport
returning astronauts to Earth
|
|
gptkbp:recovery_method
|
helicopter support
land or water
|
|
gptkbp:reliability
|
very high
|
|
gptkbp:safety_measures
|
extensive pre-flight testing
|
|
gptkbp:safety_record
|
high
|
|
gptkbp:speed
|
28,000 km/h
|
|
gptkbp:successor
|
gptkb:Soyuz_MS
|
|
gptkbp:team
|
gptkb:Russian_military
|
|
gptkbp:used_by
|
gptkb:Russian_space_agency
|
|
gptkbp:used_in
|
International Space Station missions
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_TMA
gptkb:Soyuz_MS-76
|
|
gptkbp:bfsLayer
|
5
|