|
gptkbp:instanceOf
|
gptkb:satellite
|
|
gptkbp:countryOfOrigin
|
gptkb:Russia
|
|
gptkbp:designLife
|
200 days in orbit
|
|
gptkbp:diameter
|
2.72 m
|
|
gptkbp:firstFlight
|
gptkb:Soyuz_TMA-1
2002-10-30
|
|
gptkbp:improves
|
gptkb:Soyuz_TM_spacecraft
|
|
gptkbp:lastFlight
|
gptkb:Soyuz_TMA-22
2011-11-14
|
|
gptkbp:launchMass
|
7,200 kg
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz-FG
|
|
gptkbp:length
|
7.48 m
|
|
gptkbp:manufacturer
|
gptkb:RKK_Energia
|
|
gptkbp:missionType
|
gptkb:crewed_spaceflight
|
|
gptkbp:notableFeature
|
upgraded avionics
digital flight control system
improved crew accommodation for taller astronauts
|
|
gptkbp:numberBuilt
|
12
|
|
gptkbp:operatedBy
|
gptkb:Roscosmos
|
|
gptkbp:partOf
|
gptkb:Soyuz_program
|
|
gptkbp:precededBy
|
gptkb:Soyuz_TM_spacecraft
|
|
gptkbp:seatingCapacity
|
3
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Soyuz_TMA-M_spacecraft
|
|
gptkbp:usedFor
|
International Space Station transport
crew rotation
emergency escape vehicle
|
|
gptkbp:bfsParent
|
gptkb:TMA-05M
gptkb:Soyuz-2_launches
|
|
gptkbp:bfsLayer
|
8
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz TMA spacecraft
|