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gptkbp:instanceOf
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gptkb:spacecraft
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gptkbp:communicationEquipment
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VHF radio
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gptkbp:communitySupport
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closed-loop system
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gptkbp:constructionStarted
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real-time telemetry
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gptkbp:controls
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gptkb:Moscow_Mission_Control
automatic and manual
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gptkbp:coolingSystem
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phenolic resin
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gptkbp:crew
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gptkb:Gennady_Padalka
gptkb:Joe_Acaba
gptkb:Yuri_Malyshev
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gptkbp:crewCapacity
|
3
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gptkbp:curbWeight
|
2,500 kg
|
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gptkbp:descendant
|
parachute recovery
Zhezkazgan
|
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gptkbp:firstFlight
|
2012
2012-09-17
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gptkbp:hasPostalCode
|
museum display
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gptkbp:historicalLegacy
|
contributed to human spaceflight
|
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gptkbp:historicalSignificance
|
part of ISS program
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|
https://www.w3.org/2000/01/rdf-schema#label
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Soyuz TMA-04M descent module
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gptkbp:isVulnerableTo
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ablative heat shield
|
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gptkbp:landingGear
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gptkb:Kazakhstan
shock-absorbing legs
three main parachutes
|
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gptkbp:launchDate
|
2012-05-15
|
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gptkbp:launched
|
gptkb:Soyuz_rocket
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
|
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gptkbp:launchVehicle
|
gptkb:Soyuz-FG
|
|
gptkbp:learnsMove
|
launch escape system
return_to_Earth
|
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gptkbp:manufacturer
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gptkb:RSC_Energia
|
|
gptkbp:mission
|
crewed spaceflight
|
|
gptkbp:missions
|
124 days
|
|
gptkbp:missionsConducted
|
gptkb:Soyuz_TMA-04M_patch
|
|
gptkbp:navigationEquipment
|
inertial navigation system
|
|
gptkbp:orbitalInclination
|
51.6 degrees
|
|
gptkbp:partOf
|
Soyuz_TMA-04M_mission
|
|
gptkbp:powers
|
battery powered
|
|
gptkbp:reduces
|
2.2 m diameter
|
|
gptkbp:renovated
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gptkb:Russian_Space_Agency
|
|
gptkbp:respondsTo
|
capsule
|
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gptkbp:speed
|
7.5 km/s
|
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gptkbp:successor
|
gptkb:Soyuz_TMA-05M
|
|
gptkbp:travelTime
|
ballistic
|
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gptkbp:trimLevels
|
7,200 kg
10 m³
|