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gptkbp:instance_of
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gptkb:spacecraft
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gptkbp:air_traffic_control
|
manual and automatic modes
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gptkbp:communication_system
|
S-band radio
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gptkbp:control_system
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gptkb:navigation_system
|
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gptkbp:cooling_system
|
phenolic resin
ablative heat shield
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gptkbp:crew
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gptkb:Sergey_Ryzhikov
gptkb:Andrey_Babkin
gptkb:Shane_Kimbrough
November 2, 2016
April 10, 2017
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gptkbp:crew_capacity
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gptkb:3
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gptkbp:diameter
|
2.2 m
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gptkbp:emergency_services
|
ballistic parachute
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gptkbp:first_flight
|
gptkb:Soyuz_MS-01
gptkb:Soyuz_MS-03
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gptkbp:fuel_type
|
hypergolic propellant
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gptkbp:homeworld
|
April 10, 2017
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|
https://www.w3.org/2000/01/rdf-schema#label
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Soyuz MS-02 descent module
|
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gptkbp:landing_distance
|
three main parachutes
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gptkbp:landing_site
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gptkb:Kazakhstan
|
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gptkbp:launch_site
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gptkb:Baikonur_Cosmodrome
|
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gptkbp:launch_vehicle
|
gptkb:Soyuz-FG
|
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gptkbp:launched
|
gptkb:Russian_space_agency
November 2, 2016
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gptkbp:length
|
2.5 m
|
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gptkbp:life_support_system
|
closed-loop system
|
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gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mission
|
ISS crew rotation
|
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gptkbp:mission_duration
|
173 days
|
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gptkbp:mission_type
|
gptkb:human_spaceflight
|
|
gptkbp:module
|
ballistic descent
part of Soyuz spacecraft
|
|
gptkbp:navigation_system
|
GPS and star trackers
|
|
gptkbp:operational_since
|
gptkb:2016
|
|
gptkbp:operational_status
|
retired
|
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gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:part_of
|
Soyuz MS-02 mission
|
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gptkbp:power_source
|
solar panels
|
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gptkbp:predecessor
|
gptkb:Soyuz_MS-01
|
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gptkbp:speed
|
7.5 km/s
|
|
gptkbp:status
|
decommissioned
|
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gptkbp:successor
|
gptkb:Soyuz_MS-03
|
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gptkbp:team
|
Russian recovery forces
|
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gptkbp:used_for
|
transporting crew to the ISS
|
|
gptkbp:weight
|
7,200 kg
|
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gptkbp:bfsParent
|
gptkb:Soyuz_MS-02
|
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gptkbp:bfsLayer
|
5
|