|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:communicationEquipment
|
S-band and UHF
|
|
gptkbp:controls
|
fly-by-wire
|
|
gptkbp:coolingSystem
|
Phenolic-impregnated carbon ablator
|
|
gptkbp:crew
|
gptkb:Oleg_Novitskiy
gptkb:Yuri_Malyshev
gptkb:Chris_Hadfield
|
|
gptkbp:crewCapacity
|
3
launch escape system
|
|
gptkbp:diameter
|
2.2 m
|
|
gptkbp:diedIn
|
180 days
|
|
gptkbp:environmentalImpact
|
multi-layer insulation
|
|
gptkbp:firstFlight
|
gptkb:Soyuz_MS-19
gptkb:Soyuz_TMA-1
March 16, 2013
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz TMA-50 descent module
|
|
gptkbp:landingGear
|
three main parachutes
|
|
gptkbp:launchDate
|
December 19, 2012
|
|
gptkbp:launched
|
gptkb:Russian_Federal_Space_Agency
December 2012
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
7,200 kg
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz-FG
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mission
|
crewed spaceflight
|
|
gptkbp:missions
|
108 days
|
|
gptkbp:navigationEquipment
|
Inertial navigation system
|
|
gptkbp:operationalStatus
|
retired
|
|
gptkbp:orbitalInclination
|
90 minutes
|
|
gptkbp:partOf
|
Soyuz_TMA-50_mission
|
|
gptkbp:postRetirementCareer
|
decommissioned
|
|
gptkbp:renovated
|
gptkb:Kazakhstan
Russian_Search_and_Recovery_Service
|
|
gptkbp:rootSystem
|
automatic and manual
|
|
gptkbp:services
|
Soyuz_TMA-50_service_module
|
|
gptkbp:speed
|
28,000 km/h
|
|
gptkbp:succeededBy
|
100%
|
|
gptkbp:topSpeed
|
7 m/s
|
|
gptkbp:tourism
|
gptkb:International_Space_Station
|
|
gptkbp:travelTime
|
ballistic descent
|
|
gptkbp:weight
|
7,200 kg
|