|
gptkbp:instanceOf
|
descent module
|
|
gptkbp:airlines
|
suborbital_trajectory
|
|
gptkbp:communicationEquipment
|
VHF radio
|
|
gptkbp:controls
|
automatic and manual
|
|
gptkbp:coolingSystem
|
phenolic resin
|
|
gptkbp:crew
|
gptkb:Alexander_Gerst
gptkb:Oleg_Novitskiy
gptkb:Mark_T._Vande_Hei
extensive pre-flight training
|
|
gptkbp:crewCapacity
|
3
launch escape system
|
|
gptkbp:crewSize
|
excellent
side-by-side seating
|
|
gptkbp:design
|
modular design
|
|
gptkbp:diedIn
|
closed-loop life support
|
|
gptkbp:emergencyServices
|
ballistic recovery system
detailed in crew manual
|
|
gptkbp:environmentalImpact
|
ablative heat shield
|
|
gptkbp:firstFlight
|
gptkb:Soyuz_MS-4
gptkb:Soyuz_MS-1
September 3, 2017
11:36 UTC
|
|
gptkbp:historicalSignificance
|
part of ISS crew rotation
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz MS-4 descent module
|
|
gptkbp:internationalCooperation
|
involved_NASA_and_ESA
|
|
gptkbp:landingGear
|
gptkb:Kazakhstan
three main parachutes
|
|
gptkbp:launchDate
|
April 20, 2017
11:13 UTC
|
|
gptkbp:launched
|
high
April 20, 2017
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
approximately 7,200 kg
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz-FG
|
|
gptkbp:manufacturer
|
gptkb:Russian_Federal_Space_Agency
|
|
gptkbp:mission
|
crewed spaceflight
|
|
gptkbp:missions
|
successful
approximately 5 months
fly-by-wire system
|
|
gptkbp:missionsConducted
|
Soyuz_MS-4_mission_patch
|
|
gptkbp:navigationEquipment
|
inertial navigation system
|
|
gptkbp:operationalHistory
|
part_of_the_Soyuz_program
|
|
gptkbp:operationalStatus
|
retired
|
|
gptkbp:orbitalInclination
|
51.6 degrees
|
|
gptkbp:partOf
|
Soyuz_MS-4_spacecraft
|
|
gptkbp:postRetirementCareer
|
medical checks and debriefing
|
|
gptkbp:predecessor
|
gptkb:Soyuz_MS-3
|
|
gptkbp:renovated
|
gptkb:Kazakhstan_recovery_forces
near_Zhezkazgan
|
|
gptkbp:respondsTo
|
gptkb:International_Space_Station
approximately 1.5 degrees
|
|
gptkbp:safetyFeatures
|
redundant systems
|
|
gptkbp:secondaryMission
|
conducted_by_Roscosmos
published_by_Roscosmos
|
|
gptkbp:services
|
Soyuz_MS-4_service_module
|
|
gptkbp:speed
|
approximately 7.5 km/s
|
|
gptkbp:successor
|
gptkb:Soyuz_MS-5
|
|
gptkbp:travelTime
|
approximately 2,500 kg
ballistic descent
|
|
gptkbp:trimLevels
|
approximately 10 m³
|