|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:communicationEquipment
|
radio
|
|
gptkbp:controls
|
automatic and manual
|
|
gptkbp:coolingSystem
|
ablative material
|
|
gptkbp:crewCapacity
|
3
yes
|
|
gptkbp:design
|
gptkb:Soviet_Union
|
|
gptkbp:designedFor
|
human spaceflight
|
|
gptkbp:diameter
|
2.2 meters
|
|
gptkbp:diedIn
|
yes
|
|
gptkbp:emergencyServices
|
ballistic descent
|
|
gptkbp:environmentalImpact
|
yes
|
|
gptkbp:firstDeployment
|
10,000 feet
|
|
gptkbp:firstFlight
|
1967
|
|
gptkbp:historicalSignificance
|
first crewed spacecraft to land safely after reentry.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz descent module
|
|
gptkbp:internationalCooperation
|
yes
|
|
gptkbp:landingGear
|
parachute
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz_rocket
|
|
gptkbp:length
|
2.5 meters
|
|
gptkbp:navigationEquipment
|
inertial navigation
|
|
gptkbp:notableFeature
|
ISS missions
|
|
gptkbp:numberOfFigures
|
over 150
|
|
gptkbp:operationalStatus
|
1967
active
|
|
gptkbp:partOf
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:postRetirementCareer
|
crew extraction
|
|
gptkbp:renovated
|
search and rescue team
land or water
|
|
gptkbp:respondsTo
|
1.2 degrees
|
|
gptkbp:safetyFeatures
|
redundant systems
|
|
gptkbp:services
|
gptkb:Soyuz_service_module
|
|
gptkbp:speed
|
7.5 km/s
|
|
gptkbp:succeededBy
|
high
|
|
gptkbp:training
|
simulator training
|
|
gptkbp:usedBy
|
gptkb:Russian_space_agency
|
|
gptkbp:weight
|
2,500 kg
|