|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:communicationEquipment
|
VHF radio
|
|
gptkbp:controls
|
inertial navigation system
|
|
gptkbp:coolingSystem
|
phenolic resin
|
|
gptkbp:crew
|
gptkb:Andreas_Mogensen
gptkb:Oleg_Kononenko
gptkb:Sergey_Revin
approximately 3 hours
|
|
gptkbp:crewCapacity
|
3
yes
|
|
gptkbp:diameter
|
2.2 m
|
|
gptkbp:diedIn
|
closed-loop system
|
|
gptkbp:emergencyServices
|
ballistic parachute
|
|
gptkbp:environmentalImpact
|
ablative heat shield
|
|
gptkbp:firstFlight
|
gptkb:Soyuz_MS-10
gptkb:Soyuz_TMA-1
2012-07-01
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz TMA-80 descent module
|
|
gptkbp:landingGear
|
main and reserve parachutes
|
|
gptkbp:launchDate
|
2011-12-21
|
|
gptkbp:launched
|
gptkb:Russian_Federal_Space_Agency
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
7,200 kg
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz_FG
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:missions
|
manual and automatic
165 days
|
|
gptkbp:operationalHistory
|
part of ISS missions
|
|
gptkbp:operationalStatus
|
retired
|
|
gptkbp:orbitalInclination
|
yes
|
|
gptkbp:partOf
|
Soyuz_TMA-80_mission
|
|
gptkbp:postRetirementCareer
|
decommissioned
|
|
gptkbp:renovated
|
gptkb:Kazakhstan
soft landing
Russian_recovery_forces
|
|
gptkbp:safetyFeatures
|
multiple redundancy
|
|
gptkbp:secondaryMission
|
return_to_Earth
|
|
gptkbp:services
|
yes
|
|
gptkbp:speed
|
7.5 km/s
|
|
gptkbp:succeededBy
|
high
|
|
gptkbp:tourism
|
gptkb:International_Space_Station
|
|
gptkbp:travelTime
|
yes
ballistic
|
|
gptkbp:weight
|
7,200 kg
|