|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:communicationEquipment
|
S-band
|
|
gptkbp:controls
|
automatic and manual control
|
|
gptkbp:crew
|
gptkb:Dmitry_Kondratyev
gptkb:Catherine_Coleman
gptkb:Shannon_Walker
|
|
gptkbp:crewCapacity
|
3
launch escape system
safe_return_to_Earth
|
|
gptkbp:diameter
|
2.2 m
|
|
gptkbp:diedIn
|
closed-loop system
|
|
gptkbp:environmentalImpact
|
ablative heat shield
|
|
gptkbp:finalDisposal
|
1,000 m
|
|
gptkbp:firstDeployment
|
10,000 m
|
|
gptkbp:firstFlight
|
1
June 24, 2011
December 20, 2010
|
|
gptkbp:height
|
2.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz TMA-19 descent module
|
|
gptkbp:landingGear
|
gptkb:Kazakhstan
|
|
gptkbp:launchDate
|
December 20, 2010
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
7,200 kg
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz-FG
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mission
|
crewed spaceflight
|
|
gptkbp:missions
|
180 days
|
|
gptkbp:navigationEquipment
|
inertial navigation
|
|
gptkbp:operationalStatus
|
retired
|
|
gptkbp:orbitalInclination
|
51.6 degrees
|
|
gptkbp:postRetirementCareer
|
on display
|
|
gptkbp:powers
|
solar panels
|
|
gptkbp:predecessor
|
gptkb:Soyuz_TMA-18
|
|
gptkbp:relatedPatent
|
Expedition 32
Expedition 26
Expedition 34
Expedition 35
Expedition 27
Expedition 28
Expedition 29
Expedition 30
Expedition 31
Expedition 33
|
|
gptkbp:renovated
|
parachute
|
|
gptkbp:respondsTo
|
2,500 kg
ballistic reentry
|
|
gptkbp:slopeRating
|
7 m/s
|
|
gptkbp:successor
|
gptkb:Soyuz_TMA-20
|
|
gptkbp:tourism
|
gptkb:International_Space_Station
|
|
gptkbp:trimLevels
|
after orbital maneuvering
|