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gptkbp:instanceOf
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gptkb:spacecraft
|
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gptkbp:commandStructure
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gptkb:Soyuz_MS_series
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|
gptkbp:communicationEquipment
|
S-band and UHF
|
|
gptkbp:crew
|
gptkb:Andrew_R._Morgan
gptkb:Oleg_Novitskiy
gptkb:Christina_Koch
extensive training required
|
|
gptkbp:crewCapacity
|
gptkb:Earth
3
launch escape system
|
|
gptkbp:currentStatus
|
retired from service
|
|
gptkbp:diameter
|
2.7 m
|
|
gptkbp:diedIn
|
closed-loop system
|
|
gptkbp:duration
|
180 days
|
|
gptkbp:emergencyServices
|
land_in_Kazakhstan
|
|
gptkbp:environmentalImpact
|
ablative heat shield
|
|
gptkbp:firstFlight
|
gptkb:Soyuz_1
1967
over 140
April 17, 2020
ongoing missions
|
|
gptkbp:hasPartnershipsWith
|
NASA,_ESA,_Roscosmos
|
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gptkbp:height
|
8.4 m
|
|
gptkbp:historicalSignificance
|
longest-serving crewed spacecraft
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz MS-30 capsule
|
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gptkbp:launchDate
|
November 20, 2019
|
|
gptkbp:launched
|
approximately 2-3 per year
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
7,200 kg
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz_2.1a
|
|
gptkbp:manufacturer
|
gptkb:Russian_Federal_Space_Agency
|
|
gptkbp:mission
|
crewed mission
|
|
gptkbp:navigationEquipment
|
inertial navigation system
|
|
gptkbp:operationalStatus
|
1967
retired
|
|
gptkbp:orbitalInclination
|
51.6 degrees
|
|
gptkbp:payloadCapacity
|
300 kg to ISS
|
|
gptkbp:powers
|
solar panels
|
|
gptkbp:predecessor
|
gptkb:Soyuz_MS-29
|
|
gptkbp:propulsion
|
hypergolic propellant
|
|
gptkbp:reliability
|
high reliability rate
|
|
gptkbp:respondsTo
|
heat shield
|
|
gptkbp:safetyFeatures
|
no fatalities in crewed missions
|
|
gptkbp:services
|
gptkb:Soyuz_MS_series
|
|
gptkbp:significantEvent
|
first female crew member in 1982
|
|
gptkbp:successor
|
gptkb:Soyuz_MS-31
|
|
gptkbp:tourism
|
gptkb:International_Space_Station
|
|
gptkbp:travelTime
|
gptkb:Soyuz_MS_series
|
|
gptkbp:type
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:weight
|
7,200 kg
|