gptkbp:instanceOf
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gptkb:spacecraft
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gptkbp:CEO
|
2
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gptkbp:communicationEquipment
|
S-band
UHF_and_VHF
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gptkbp:controls
|
fly-by-wire
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gptkbp:crew
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gptkb:Alexander_Gerst
gptkb:Oleg_Novitskiy
gptkb:Mark_T._Vande_Hei
real-time monitoring
extensive training
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gptkbp:crewCapacity
|
3
splashdown
varied backgrounds
launch escape system
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gptkbp:crewSize
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international selection process
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gptkbp:diedIn
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closed-loop system
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gptkbp:emergencyServices
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detailed protocols
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gptkbp:environmentalImpact
|
active and passive
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gptkbp:firstAwarded
|
APAS
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gptkbp:firstFlight
|
2023-04-15
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gptkbp:height
|
3.4 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz MS-3
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gptkbp:internationalCooperation
|
NASA,_ESA,_Roscosmos
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gptkbp:landingGear
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gptkb:Kazakhstan
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gptkbp:launchDate
|
2023-04-15
12:00 UTC
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gptkbp:launched
|
April 2023
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gptkbp:launchSite
|
Baikonur Cosmodrome
7,200 kg
|
gptkbp:launchVehicle
|
gptkb:Soyuz-2.1b
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gptkbp:length
|
7.2 m
|
gptkbp:manufacturer
|
gptkb:Russian_Federal_Space_Agency
|
gptkbp:mission
|
crewed
|
gptkbp:missions
|
gptkb:Moscow_Mission_Control_Center
6 months
autonomous and manual
ISS resupply
|
gptkbp:missionsConducted
|
Soyuz_MS-3_mission_patch
|
gptkbp:navigationEquipment
|
inertial navigation
|
gptkbp:operationalStatus
|
2023-04-15
|
gptkbp:orbitalInclination
|
Low Earth Orbit
90 minutes
51.6 degrees
|
gptkbp:payloadCapacity
|
100 kg to ISS
|
gptkbp:powerOutput
|
1,000 W
|
gptkbp:renovated
|
parachute
|
gptkbp:respondsTo
|
descent module
|
gptkbp:safetyFeatures
|
redundant systems
|
gptkbp:scientificName
|
multiple experiments conducted
|
gptkbp:secondaryMission
|
gptkb:Soyuz_MS-4
gptkb:Soyuz_MS-2
detailed analysis conducted
|
gptkbp:services
|
service module
|
gptkbp:speed
|
28,000 km/h
|
gptkbp:status
|
active
|
gptkbp:successor
|
gptkb:Soyuz_MS-4
|
gptkbp:tourism
|
gptkb:International_Space_Station
|
gptkbp:training
|
6 months
|
gptkbp:weight
|
7,200 kg
|
gptkbp:width
|
2.7 m
|
gptkbp:yearEstablished
|
2023-10-15
|