|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:capacity
|
3 crew members
|
|
gptkbp:CEO
|
2
|
|
gptkbp:communicationEquipment
|
digital communication system
|
|
gptkbp:controls
|
digital fly-by-wire
|
|
gptkbp:crew
|
gptkb:Gagarin_Cosmonaut_Training_Center
|
|
gptkbp:crewCapacity
|
3
yes
ballistic parachute
|
|
gptkbp:designedBy
|
gptkb:Russian_Federal_Space_Agency
|
|
gptkbp:developer
|
2016
|
|
gptkbp:diameter
|
2.7 m
|
|
gptkbp:diedIn
|
closed-loop system
|
|
gptkbp:emergencyServices
|
launch escape system
|
|
gptkbp:environmentalImpact
|
ablative heat shield
|
|
gptkbp:firstFlight
|
2021-10-05
over 10
2016-11-17
|
|
gptkbp:hasPartnershipsWith
|
NASA,_ESA,_JAXA
|
|
gptkbp:historicalSignificance
|
longest-running crewed spacecraft series
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz MS series
|
|
gptkbp:isUpdatedBy
|
2021
|
|
gptkbp:landingGear
|
parachute system
|
|
gptkbp:launched
|
approximately $50 million
approximately 2-3 per year
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz-2.1b
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:manufacturer
|
gptkb:Progress_Rocket_Space_Centre
|
|
gptkbp:missions
|
gptkb:Moscow_Mission_Control_Center
up to 6 months
|
|
gptkbp:navigationEquipment
|
inertial navigation system
|
|
gptkbp:notableFeature
|
Expedition 50/51
|
|
gptkbp:operationalStatus
|
2016
active
|
|
gptkbp:orbitalInclination
|
approximately 400 km
|
|
gptkbp:passenger_traffic
|
yes
|
|
gptkbp:passengerCapacity
|
up to 500 kg
|
|
gptkbp:productionCompany
|
2012
|
|
gptkbp:propulsion
|
RD-107A_engines
|
|
gptkbp:releaseFormat
|
Gagarin_Launch_Complex
|
|
gptkbp:reliability
|
not_reusable
|
|
gptkbp:respondsTo
|
yes
|
|
gptkbp:safetyFeatures
|
high safety record
|
|
gptkbp:services
|
yes
|
|
gptkbp:successor
|
gptkb:Soyuz_2.1a
|
|
gptkbp:technology
|
advanced telemetry system
|
|
gptkbp:usedFor
|
transporting_crew_to_the_International_Space_Station
|
|
gptkbp:weight
|
approximately 7,200 kg
|