|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:aircraft_operated
|
up to 6 months
|
|
gptkbp:cargo_types
|
limited cargo capacity
|
|
gptkbp:collaboration
|
gptkb:JAXA
gptkb:ISS_program
gptkb:ESA
gptkb:NASA
|
|
gptkbp:communication_system
|
radio communication
|
|
gptkbp:control_system
|
digital
|
|
gptkbp:cooling_system
|
ablative heat shield
|
|
gptkbp:crew
|
gptkb:Oleg_Kononenko
gptkb:Alexey_Ovchinin
gptkb:Valentina_Tereshkova
gptkb:Yuri_Gagarin
gptkb:Jessica_Meir
gptkb:launch_escape_system
simulator training
comfortable seating
several months
high safety standards
emergency escape system
NASA and Roscosmos astronauts
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:current_condition
|
gptkb:Roscosmos
|
|
gptkbp:data_return
|
splashdown
|
|
gptkbp:debut
|
over 150 launches since 1967
|
|
gptkbp:design_features
|
modular design
|
|
gptkbp:docking_system
|
gptkb:Androgynous
|
|
gptkbp:emergency_services
|
well-defined protocols
|
|
gptkbp:first_flight
|
2016-11-17
|
|
gptkbp:flight_style
|
over 20
|
|
gptkbp:historical_significance
|
longest-serving crewed spacecraft
|
|
gptkbp:homeworld
|
parachute landing
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz MS spacecraft
|
|
gptkbp:launch_date
|
approximately 2-3 per year
|
|
gptkbp:launch_mass
|
7,200 kg
|
|
gptkbp:launch_platform
|
gptkb:Baikonur_launch_control_center
|
|
gptkbp:launch_price
|
approximately $50 million
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz-2.1a
|
|
gptkbp:life_support_system
|
environmental control system
|
|
gptkbp:lifespan
|
approximately 6 months
|
|
gptkbp:manufacturer
|
gptkb:Russian_Federal_Space_Agency
|
|
gptkbp:mission_duration
|
gptkb:Apollo-Soyuz_Test_Project
|
|
gptkbp:mission_type
|
gptkb:transportation
|
|
gptkbp:next_edition
|
gptkb:Soyuz_MS-20
gptkb:Soyuz_TMA
|
|
gptkbp:notable_mission
|
ISS crew transport
|
|
gptkbp:operational_since
|
gptkb:2000
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:orbital_altitude
|
400 km
yes
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:origin
|
gptkb:Soviet_Union
|
|
gptkbp:payload_capacity
|
up to 500 kg to ISS
|
|
gptkbp:safety_record
|
high reliability
|
|
gptkbp:service
|
gptkb:Public_service
|
|
gptkbp:speed
|
gptkb:Lunar_Module
28,000 km/h
|
|
gptkbp:successor
|
gptkb:Soyuz_MS-19
|
|
gptkbp:team
|
search and rescue team
|
|
gptkbp:type
|
gptkb:spacecraft
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_MS-15
gptkb:Soyuz_MS-93
gptkb:Soyuz_MS-98
gptkb:Soyuz_MS-06
gptkb:Soyuz_MS-91
gptkb:Soyuz_MS-66
gptkb:Soyuz_MS-73
gptkb:Soyuz_MS-68
gptkb:Soyuz_MS-36
gptkb:Soyuz_MS-61
|
|
gptkbp:bfsLayer
|
5
|