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gptkbp:instanceOf
|
spacecraft design
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|
gptkbp:armament
|
ablative
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|
gptkbp:communication
|
VHF/UHF radio
|
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gptkbp:containsModule
|
gptkb:Service_Module
Descent Module
Orbital Module
|
|
gptkbp:countryOfOrigin
|
gptkb:Russia
gptkb:Soviet_Union
|
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gptkbp:designer
|
gptkb:Sergei_Korolev
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gptkbp:diameter
|
2.72 m
|
|
gptkbp:dockedWith
|
probe and drogue
|
|
gptkbp:duration
|
up to 215 days (docked)
|
|
gptkbp:escapeMethod
|
launch escape system
|
|
gptkbp:firstFlight
|
1967
|
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gptkbp:guidanceSystem
|
inertial and radio guidance
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz spacecraft design
|
|
gptkbp:landingSystem
|
soft-landing rockets
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz_rocket
|
|
gptkbp:length
|
7.48 m
|
|
gptkbp:lifeSupport
|
up to 30 days
|
|
gptkbp:manufacturer
|
gptkb:RKK_Energia
|
|
gptkbp:mass
|
7,200 kg
|
|
gptkbp:notableMission
|
gptkb:Apollo-Soyuz_Test_Project
first crewed ISS mission
longest single flight: Soyuz TM-9 (179 days)
|
|
gptkbp:notableVariant
|
gptkb:Soyuz-T
gptkb:Soyuz-MS
gptkb:Soyuz_7K-T
gptkb:Soyuz-TM
gptkb:Soyuz_7K-OK
gptkb:Soyuz-TMA
|
|
gptkbp:operates
|
gptkb:International_Space_Station
gptkb:Mir
Salyut stations
Almaz stations
|
|
gptkbp:parachuteSystem
|
main and reserve parachutes
|
|
gptkbp:powerSource
|
solar panels
|
|
gptkbp:reentryDate
|
ballistic reentry
|
|
gptkbp:seatingCapacity
|
3
|
|
gptkbp:status
|
active
|
|
gptkbp:usedBy
|
gptkb:NASA
gptkb:Soviet_space_program
gptkb:Russian_space_program
gptkb:Roscosmos
gptkb:ESA
|
|
gptkbp:usedFor
|
human spaceflight
crew transfer
space station transport
emergency escape vehicle
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|
gptkbp:bfsParent
|
gptkb:ShenZhou
|
|
gptkbp:bfsLayer
|
8
|