|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:communicationEquipment
|
VHF radio
|
|
gptkbp:controls
|
automatic and manual control
|
|
gptkbp:coolingSystem
|
Phenolic resin
|
|
gptkbp:crew
|
gptkb:Gennady_Padalka
gptkb:Andreas_Mogensen
gptkb:Kimiya_Yui
|
|
gptkbp:crewCapacity
|
3
ejection seats
safe_return_to_Earth
|
|
gptkbp:diameter
|
2.2 m
|
|
gptkbp:diedIn
|
closed-loop system
|
|
gptkbp:duration
|
186 days
|
|
gptkbp:emergencyServices
|
launch escape system
|
|
gptkbp:environmentalImpact
|
ablative heat shield
|
|
gptkbp:firstFlight
|
gptkb:Soyuz_MS-18
gptkb:Soyuz_TMA-1
September 11, 2015
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz TMA-64 descent module
|
|
gptkbp:internationalCooperation
|
NASA,_ESA,_JAXA
|
|
gptkbp:landingGear
|
parachute landing
three main parachutes
|
|
gptkbp:launchDate
|
April 4, 2015
|
|
gptkbp:launched
|
gptkb:Russian_Federal_Space_Agency
3 astronauts
|
|
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
|
inertial navigation system
186 days
|
|
gptkbp:operationalStatus
|
2003
retired
|
|
gptkbp:orbitalInclination
|
51.6 degrees
|
|
gptkbp:partOf
|
Soyuz_TMA-64_mission
|
|
gptkbp:powers
|
solar panels
|
|
gptkbp:renovated
|
gptkb:Kazakhstan
soft landing
|
|
gptkbp:respondsTo
|
gptkb:Soyuz_TMA-64
|
|
gptkbp:secondaryMission
|
over 140
return_to_Earth
|
|
gptkbp:significantEvent
|
first Danish astronaut
first Japanese astronaut on ISS
longest_mission_for_Gennady_Padalka
|
|
gptkbp:speed
|
7.5 km/s
|
|
gptkbp:successor
|
gptkb:Soyuz_MS-01
|
|
gptkbp:tourism
|
gptkb:International_Space_Station
|
|
gptkbp:travelTime
|
ballistic descent
|
|
gptkbp:weight
|
7,200 kg
|