gptkbp:instanceOf
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gptkb:spacecraft
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gptkbp:aircraft
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2.2 m
7.2 m
3.4 m
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gptkbp:communicationEquipment
|
S-band
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gptkbp:controls
|
fly-by-wire system
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gptkbp:crew
|
gptkb:Samantha_Cristoforetti
gptkb:Andrey_Babkin
Commander
Alexander Samokutyayev
Flight_Engineer
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gptkbp:crewCapacity
|
gptkb:Soyuz_TMA_Descent_Module
Italian
Russian
launch escape system
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gptkbp:crewSize
|
3
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gptkbp:diedIn
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closed-loop system
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gptkbp:duration
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168 days
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gptkbp:environmentalImpact
|
ablative heat shield
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gptkbp:firstAwarded
|
2017-02-01
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gptkbp:firstFlight
|
09:15 UTC
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https://www.w3.org/2000/01/rdf-schema#label
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Soyuz TMA-85
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gptkbp:landingGear
|
gptkb:Kazakhstan
2,500 kg
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gptkbp:launchDate
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2014-09-25
01:25 UTC
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gptkbp:launchSite
|
Baikonur Cosmodrome
7,200 kg
|
gptkbp:launchVehicle
|
gptkb:Soyuz_FG
|
gptkbp:mission
|
gptkb:Soyuz_TMA
crewed mission
|
gptkbp:missions
|
5 months
completed
|
gptkbp:missionsConducted
|
https://upload.wikimedia.org/wikipedia/commons/5/5e/Soyuz_TMA-85_patch.png
|
gptkbp:navigationEquipment
|
inertial navigation system
|
gptkbp:notableFeature
|
2003-11-20
|
gptkbp:operator
|
gptkb:Russian_Federal_Space_Agency
|
gptkbp:orbitalInclination
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gptkb:Soyuz_TMA_Orbital_Module
90 minutes
51.6 degrees
|
gptkbp:powers
|
solar panels
|
gptkbp:predecessor
|
gptkb:Soyuz_TMA-84
|
gptkbp:propulsion
|
hypergolic propellant
|
gptkbp:services
|
gptkb:Soyuz_Service_Module
gptkb:Soyuz_Descent_Module
gptkb:Soyuz_Orbital_Module
gptkb:Soyuz_TMA_Service_Module
|
gptkbp:speed
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28,000 km/h
|
gptkbp:successor
|
gptkb:Soyuz_MS-01
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gptkbp:tourism
|
gptkb:International_Space_Station
|
gptkbp:travelTime
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gptkb:Soyuz_TMA_Descent_Module
|
gptkbp:weight
|
7,200 kg
|
gptkbp:yearEstablished
|
2015-03-11
|