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gptkbp:instanceOf
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gptkb:spacecraft
|
|
gptkbp:communicationEquipment
|
S-band and UHF
|
|
gptkbp:controls
|
Fly-by-wire system
|
|
gptkbp:coolingSystem
|
Phenolic-impregnated carbon ablator
|
|
gptkbp:crew
|
gptkb:Kazakhstan
gptkb:Oleg_Novitskiy
gptkb:Mark_T._Vande_Hei
gptkb:Sergey_Korsakov
2021-04-17
|
|
gptkbp:crewCapacity
|
3
Launch escape system
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|
gptkbp:design
|
180 days
|
|
gptkbp:diameter
|
2.7 m
|
|
gptkbp:diedIn
|
Closed-loop system
|
|
gptkbp:environmentalImpact
|
Multi-layer insulation
|
|
gptkbp:firstFlight
|
gptkb:Soyuz_1
gptkb:Soyuz_MS-46
|
|
gptkbp:fuelType
|
Hydrazine
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz MS-46 Descent Module
|
|
gptkbp:landingGear
|
gptkb:Kazakhstan
Parachute landing
Three main parachutes
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|
gptkbp:launched
|
gptkb:Oleg_Novitskiy
gptkb:Mark_T._Vande_Hei
gptkb:Sergey_Korsakov
Baikonur Cosmodrome
April 2021
2021-04-09
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
7,200 kg
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz-2.1a
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mission
|
International_Space_Station_resupply
|
|
gptkbp:missions
|
12 days
|
|
gptkbp:missionsConducted
|
gptkb:Soyuz_MS-46_patch
|
|
gptkbp:navigationEquipment
|
Inertial navigation system
|
|
gptkbp:operatedBy
|
gptkb:Roscosmos
|
|
gptkbp:operationalStatus
|
Retired
|
|
gptkbp:orbitalInclination
|
51.6 degrees
|
|
gptkbp:partOf
|
Soyuz_MS-46_mission
|
|
gptkbp:powers
|
Solar panels
|
|
gptkbp:predecessor
|
gptkb:Soyuz_MS-47
|
|
gptkbp:renovated
|
gptkb:Kazakhstan
gptkb:Kazakhstan_recovery_forces
|
|
gptkbp:respondsTo
|
gptkb:Oleg_Novitskiy
gptkb:Mark_T._Vande_Hei
gptkb:Sergey_Korsakov
2021-04-17
1.2 degrees
|
|
gptkbp:successor
|
gptkb:Soyuz_MS-45
|
|
gptkbp:travelTime
|
7.5 km/h
Ballistic_descent
|
|
gptkbp:usedFor
|
human spaceflight
|
|
gptkbp:weight
|
2,500 kg
|