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gptkbp:instanceOf
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gptkb:spacecraft
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gptkbp:airlines
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suborbital_trajectory
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gptkbp:communicationEquipment
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VHF radio
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gptkbp:controls
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automatic and manual
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gptkbp:coolingSystem
|
Phenolic resin
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gptkbp:crew
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gptkb:Sergei_Krikalev
gptkb:William_Shepherd
extensive pre-flight training
Yuri Gidzenko
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gptkbp:crewCapacity
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3
launch escape system
returned_safely_to_Earth
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gptkbp:design
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transport crew to and from space
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gptkbp:diameter
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2.2 m
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gptkbp:diedIn
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closed-loop system
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gptkbp:emergencyServices
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ballistic landing
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gptkbp:environmentalImpact
|
ablative heat shield
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gptkbp:firstFlight
|
gptkb:Soyuz_MS-19
gptkb:Soyuz_TM-1
2000-04-18
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gptkbp:historicalSignificance
|
first crewed mission to ISS
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz TM-31 descent module
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gptkbp:internationalCooperation
|
NASA_and_Roscosmos
|
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gptkbp:landingGear
|
gptkb:Kazakhstan
three main parachutes
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|
gptkbp:launchDate
|
1999-10-20
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gptkbp:launched
|
gptkb:Soyuz_program
high
October 1999
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
7,200 kg
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz-FG
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mission
|
manned spaceflight
|
|
gptkbp:missions
|
fly-by-wire
182 days
|
|
gptkbp:navigationEquipment
|
inertial navigation
|
|
gptkbp:operationalStatus
|
retired
|
|
gptkbp:orbitalInclination
|
51.6 degrees
|
|
gptkbp:postRetirementCareer
|
medical checks
|
|
gptkbp:powers
|
solar panels
|
|
gptkbp:renovated
|
gptkb:Russian_Space_Forces
helicopter recovery
|
|
gptkbp:respondsTo
|
6.5 degrees
|
|
gptkbp:safetyFeatures
|
multiple redundancy
|
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gptkbp:secondaryMission
|
successfully completed
|
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gptkbp:speed
|
7.5 km/s
|
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gptkbp:successor
|
gptkb:Soyuz_TM-32
|
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gptkbp:tourism
|
gptkb:International_Space_Station
|
|
gptkbp:travelTime
|
approximately 30 minutes
ballistic descent
|
|
gptkbp:weight
|
7,200 kg
|