|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:associatedWith
|
gptkb:International_Space_Station
|
|
gptkbp:communicationEquipment
|
VHF radio
|
|
gptkbp:crew
|
gptkb:Gagarin_Cosmonaut_Training_Center
Star City
over 30 astronauts
|
|
gptkbp:crewCapacity
|
3
launch escape system
|
|
gptkbp:decommissioned
|
2002
|
|
gptkbp:designedBy
|
gptkb:Soviet_Union
|
|
gptkbp:diedIn
|
closed-loop system
|
|
gptkbp:firstAwarded
|
APAS
|
|
gptkbp:firstFlight
|
12
2002
1986-1987
2002-04-25
|
|
gptkbp:height
|
2.5 m
|
|
gptkbp:historicalSignificance
|
first spacecraft to use digital avionics
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz-TM
|
|
gptkbp:influenced
|
future_Soyuz_variants
|
|
gptkbp:influencedBy
|
gptkb:Soyuz_7K-OK
|
|
gptkbp:inspiration
|
future spacecraft designs
|
|
gptkbp:internationalCooperation
|
NASA
|
|
gptkbp:involvedIn
|
scientific research missions
|
|
gptkbp:launchDate
|
1986-12-21
|
|
gptkbp:launched
|
12
annual
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz_rocket
|
|
gptkbp:legacy
|
pioneering role in human spaceflight
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mission
|
transport
manned spacecraft
|
|
gptkbp:notableFeature
|
gptkb:Mir_space_station
advanced navigation systems
|
|
gptkbp:operatedBy
|
gptkb:Roscosmos
|
|
gptkbp:operationalStatus
|
15 years
retired
|
|
gptkbp:orbitalInclination
|
90 minutes
|
|
gptkbp:partOf
|
gptkb:Soyuz_program
|
|
gptkbp:powers
|
solar panels
|
|
gptkbp:productionYears
|
1986 to 2002
|
|
gptkbp:reliability
|
high
|
|
gptkbp:respondsTo
|
gptkb:Soyuz_capsule
gptkb:Soyuz_descent_module
|
|
gptkbp:safetyFeatures
|
excellent
|
|
gptkbp:services
|
gptkb:Soyuz_service_module
|
|
gptkbp:successor
|
gptkb:Soyuz_TMA_program
gptkb:Soyuz_TMA
|
|
gptkbp:usedBy
|
gptkb:Russian_space_agency
|
|
gptkbp:usedFor
|
manned spaceflight
|
|
gptkbp:weight
|
7,200 kg
|
|
gptkbp:width
|
2.2 m
|