|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:airlines
|
suborbital_trajectory
|
|
gptkbp:communicationEquipment
|
S-band radio
|
|
gptkbp:controls
|
Inertial navigation system
|
|
gptkbp:coolingSystem
|
Phenolic-impregnated carbon ablator
|
|
gptkbp:crew
|
gptkb:Dmitry_Kondratyev
gptkb:Catherine_Coleman
gptkb:Shannon_Walker
extensive training
continuous monitoring
|
|
gptkbp:crewCapacity
|
gptkb:Soyuz_TMA-61
3
yes
pre-flight training
|
|
gptkbp:diameter
|
2.2 m
|
|
gptkbp:diedIn
|
Oxygen generation system
|
|
gptkbp:emergencyServices
|
ballistic parachute system
|
|
gptkbp:firstFlight
|
gptkb:Soyuz_MS-19
gptkb:Soyuz_TMA-1
March 16, 2011
2011-03-16T10:25:00Z
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz TMA-61 descent module
|
|
gptkbp:landingGear
|
parachute landing
main and reserve parachutes
|
|
gptkbp:launchDate
|
December 15, 2010
2010-12-15T12:09:00Z
|
|
gptkbp:launched
|
gptkb:Soyuz_rocket
2010
3
successful
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
7,200 kg
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz-FG
|
|
gptkbp:length
|
2.5 m
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mission
|
crewed spaceflight
|
|
gptkbp:missions
|
gptkb:Russian_Federal_Space_Agency
gptkb:Moscow_Mission_Control_Center
transport crew to ISS
159 days
|
|
gptkbp:missionsConducted
|
Soyuz_TMA-61_mission_patch
|
|
gptkbp:orbitalInclination
|
90 minutes
51.6 degrees
|
|
gptkbp:partOf
|
Soyuz_TMA-61_mission
|
|
gptkbp:postRetirementCareer
|
decommissioned
recovery and inspection
|
|
gptkbp:renovated
|
gptkb:Kazakhstan
Kazakh_recovery_team
|
|
gptkbp:respondsTo
|
yes
1.5 degrees
March 16, 2011
|
|
gptkbp:safetyFeatures
|
multiple redundancy systems
|
|
gptkbp:services
|
Soyuz_TMA-61_service_module
|
|
gptkbp:speed
|
28,000 km/h
|
|
gptkbp:successor
|
gptkb:Soyuz_TMA-22
|
|
gptkbp:tourism
|
gptkb:International_Space_Station
|
|
gptkbp:travelTime
|
ballistic descent
|
|
gptkbp:weight
|
7,200 kg
|