gptkbp:instanceOf
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gptkb:spacecraft
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gptkbp:aircraft
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modular design
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gptkbp:communicationEquipment
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radio communication
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gptkbp:crew
|
cosmonaut training
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gptkbp:crewCapacity
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3
launch escape system
high safety measures
safe_return_to_Earth
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gptkbp:crewSize
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life support systems
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gptkbp:currentUse
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ISS resupply missions
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gptkbp:diameter
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2.2 meters
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gptkbp:diedIn
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environmental control system
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gptkbp:emergencyServices
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detailed protocols
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gptkbp:environmentalImpact
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heat shield
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gptkbp:firstAwarded
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probe and drogue
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gptkbp:firstFlight
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gptkb:Soyuz_1
gptkb:Soyuz_MS-18
1967
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gptkbp:flora
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5.0 cubic meters
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gptkbp:futurePlans
|
upgraded versions
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gptkbp:hasPartnershipsWith
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NASA,_ESA,_Roscosmos
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gptkbp:historicalSignificance
|
first operational spacecraft
|
https://www.w3.org/2000/01/rdf-schema#label
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Soyuz orbital module
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gptkbp:internationalCooperation
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ISS missions
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gptkbp:launched
|
over 90%
ground control
approximately $60 million
frequent launches
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gptkbp:launchSite
|
Baikonur Cosmodrome
7,200 kg
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gptkbp:launchVehicle
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gptkb:Soyuz_rocket
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gptkbp:length
|
7.2 meters
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gptkbp:manufacturer
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gptkb:RSC_Energia
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gptkbp:mission
|
advanced avionics
manned spacecraft
tested and reliable
|
gptkbp:missions
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up to 6 months
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gptkbp:navigationEquipment
|
inertial navigation
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gptkbp:operationalHistory
|
over 50 years of service
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gptkbp:operationalStatus
|
1967
active
|
gptkbp:orbitalInclination
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200-400 km
90 minutes
thrusters
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gptkbp:partOf
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gptkb:Soyuz_spacecraft
|
gptkbp:payloadCapacity
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up to 500 kg
|
gptkbp:powers
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solar panels
|
gptkbp:reliability
|
proven track record
|
gptkbp:respondsTo
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gptkb:Soyuz_descent_module
controlled descent
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gptkbp:safetyFeatures
|
high safety standards
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gptkbp:scientificName
|
microgravity research
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gptkbp:services
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gptkb:Soyuz_spacecraft
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gptkbp:training
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gptkb:Gagarin_Cosmonaut_Training_Center
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gptkbp:updates
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regular upgrades
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gptkbp:usedFor
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human spaceflight
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gptkbp:weight
|
2,500 kg
|