gptkbp:instanceOf
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gptkb:spacecraft
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gptkbp:crew
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Star City
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gptkbp:crewCapacity
|
3
launch escape system
ballistic parachute
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gptkbp:currentStatus
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in service
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gptkbp:design
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three modules: orbital, service, and reentry
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gptkbp:designedBy
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gptkb:Soviet_Union
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gptkbp:diameter
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2.7 meters
|
gptkbp:diedIn
|
up to 6 months
|
gptkbp:firstAwarded
|
probe and drogue
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gptkbp:firstFlight
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gptkb:Soyuz_MS-19
gptkb:Soyuz_1
1967
over 140
|
gptkbp:hasPartnershipsWith
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NASA,_ESA,_JAXA
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gptkbp:historicalSignificance
|
first spacecraft to carry humans to space
|
https://www.w3.org/2000/01/rdf-schema#label
|
Russian Soyuz
|
gptkbp:inspiration
|
other spacecraft designs
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gptkbp:landingGear
|
parachute
|
gptkbp:launched
|
frequent
approximately $50 million
|
gptkbp:launchSite
|
Baikonur Cosmodrome
|
gptkbp:launchVehicle
|
gptkb:Soyuz_rocket
|
gptkbp:length
|
7.2 meters
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
gptkbp:mission
|
manned spacecraft
|
gptkbp:modifications
|
Soyuz_T,_Soyuz_TM,_Soyuz_MS
|
gptkbp:notableFeature
|
gptkb:International_Space_Station
|
gptkbp:notableTracks
|
Yuri_Gagarin,_Valentina_Tereshkova
|
gptkbp:operatedBy
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gptkb:Roscosmos
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gptkbp:operationalRole
|
transport to ISS
|
gptkbp:operationalStatus
|
1967
|
gptkbp:orbitalInclination
|
28,000 km/h
|
gptkbp:payloadCapacity
|
up to 2,500 kg
|
gptkbp:reliability
|
high
over 95%
|
gptkbp:respondsTo
|
controlled descent
|
gptkbp:safetyFeatures
|
one of the safest
|
gptkbp:services
|
provides life support
|
gptkbp:successor
|
gptkb:Soyuz_MS
|
gptkbp:usedFor
|
human spaceflight
|
gptkbp:weight
|
7,200 kg
|