|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:communicationEquipment
|
Radio and telemetry
|
|
gptkbp:controls
|
Automated and manual
|
|
gptkbp:crew
|
Yes
|
|
gptkbp:crewCapacity
|
3
Yes
|
|
gptkbp:decommissioned
|
Yes
|
|
gptkbp:design
|
gptkb:Soviet_Union
180 days
|
|
gptkbp:diedIn
|
Oxygen generation
|
|
gptkbp:emergencyServices
|
Yes
|
|
gptkbp:environmentalImpact
|
Active and passive
|
|
gptkbp:finaleDate
|
2017-09-13
|
|
gptkbp:firstAwarded
|
APAS
|
|
gptkbp:firstFlight
|
16
2002
2017
TMA-1
|
|
gptkbp:height
|
2.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz TMA Service Module
|
|
gptkbp:inspiration
|
Previous_Soyuz_models
|
|
gptkbp:internationalCooperation
|
NASA,_ESA,_JAXA
|
|
gptkbp:launchDate
|
2002-04-08
|
|
gptkbp:launched
|
gptkb:Russian_Federal_Space_Agency
Annual
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz_rocket
|
|
gptkbp:length
|
4.5 m
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:modifications
|
TMA-2, TMA-3
|
|
gptkbp:navigationEquipment
|
Inertial and GPS
|
|
gptkbp:notableFeature
|
ISS resupply
|
|
gptkbp:operationalStatus
|
Retired
|
|
gptkbp:orbitalInclination
|
200-400 km
90 minutes
|
|
gptkbp:partOf
|
gptkb:Soyuz_TMA
|
|
gptkbp:payloadCapacity
|
100 kg
|
|
gptkbp:powers
|
Solar panels
|
|
gptkbp:primaryFunction
|
Cargo transport
Crew transport
|
|
gptkbp:productionYears
|
6 months
|
|
gptkbp:renovated
|
gptkb:Kazakhstan
Parachute
|
|
gptkbp:respondsTo
|
Yes
|
|
gptkbp:safetyFeatures
|
High
|
|
gptkbp:successor
|
gptkb:Soyuz_MS
|
|
gptkbp:tourism
|
gptkb:International_Space_Station
|
|
gptkbp:usedFor
|
Transporting astronauts
|
|
gptkbp:weight
|
2,500 kg
|
|
gptkbp:width
|
2.2 m
|