|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:communicationEquipment
|
S-band and Ku-band
|
|
gptkbp:controls
|
digital fly-by-wire
|
|
gptkbp:coolingSystem
|
ablative material
|
|
gptkbp:crew
|
gptkb:Oleg_Novitskiy
gptkb:Mark_T._Vande_Hei
gptkb:Kimiya_Yui
|
|
gptkbp:crewCapacity
|
3
yes
launch escape system
|
|
gptkbp:design
|
6 months
|
|
gptkbp:diameter
|
2.2 m
|
|
gptkbp:diedIn
|
closed-loop system
|
|
gptkbp:duration
|
approximately 180 days
|
|
gptkbp:firstFlight
|
gptkb:Soyuz_1
gptkb:Soyuz_MS-22
|
|
gptkbp:hasVersion
|
gptkb:Soyuz_MS-20
gptkb:Soyuz_TMA
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz MS-19 capsule
|
|
gptkbp:internationalCooperation
|
NASA, Roscosmos, JAXA
|
|
gptkbp:landingGear
|
gptkb:Kazakhstan
|
|
gptkbp:launchDate
|
2021-04-09
|
|
gptkbp:launched
|
gptkb:Arianespace
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
7,200 kg
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz_2.1a
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:manufacturer
|
gptkb:Russian_Federal_Space_Agency
|
|
gptkbp:mission
|
crewed mission
|
|
gptkbp:missions
|
autonomous and manual
|
|
gptkbp:operationalStatus
|
2000
retired
|
|
gptkbp:orbitalInclination
|
51.6 degrees
|
|
gptkbp:passengerCapacity
|
up to 500 kg
|
|
gptkbp:powers
|
solar panels
|
|
gptkbp:reliability
|
partially reusable
|
|
gptkbp:renovated
|
parachute system
|
|
gptkbp:safetyFeatures
|
redundant systems
|
|
gptkbp:scientificName
|
various microgravity experiments
|
|
gptkbp:secondaryMission
|
gptkb:Soyuz_MS-18
gptkb:Soyuz_MS-20
|
|
gptkbp:succeededBy
|
over 90%
|
|
gptkbp:tourism
|
gptkb:International_Space_Station
|
|
gptkbp:weight
|
7,200 kg
|
|
gptkbp:yearEstablished
|
2021-10-17
|