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gptkbp:instanceOf
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gptkb:spacecraft
|
|
gptkbp:communicationEquipment
|
radio communication system
|
|
gptkbp:controls
|
automatic control system
|
|
gptkbp:crew
|
gptkb:Viktor_Patsayev
gptkb:Vladimir_Shatalov
gptkb:Aleksandr_Serebrov
Cosmonaut training program
|
|
gptkbp:crewCapacity
|
3
launch escape system
|
|
gptkbp:design
|
1 year
transport to space station
|
|
gptkbp:diameter
|
2.2 m
|
|
gptkbp:diedIn
|
environmental control system
|
|
gptkbp:environmentalImpact
|
heat shield
|
|
gptkbp:firstFlight
|
gptkb:Soyuz_1
3
1967-11-28
1971-10-30
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz 7K-OK
|
|
gptkbp:influencedBy
|
gptkb:Apollo_program
gptkb:Gemini_program
|
|
gptkbp:launchDate
|
1967-11-28
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
6800 kg
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz_rocket
gptkb:Soyuz_2.1a
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:manufacturer
|
gptkb:OKB-1
|
|
gptkbp:mission
|
manned spaceflight
|
|
gptkbp:missions
|
up to 30 days
|
|
gptkbp:notableFeature
|
gptkb:reusable_spacecraft
gptkb:Soyuz_11
gptkb:Soyuz_10
modular design
high reliability
long duration missions
automated docking system
crew return capability
|
|
gptkbp:operationalStatus
|
1967-1971
retired
|
|
gptkbp:orbitalInclination
|
200 km
88 minutes
51.6 degrees
|
|
gptkbp:payloadCapacity
|
1000 kg
|
|
gptkbp:powers
|
solar panels
|
|
gptkbp:predecessor
|
gptkb:Vostok_spacecraft
|
|
gptkbp:renovated
|
parachute system
|
|
gptkbp:respondsTo
|
gptkb:Soyuz_descent_module
|
|
gptkbp:secondaryMission
|
3
|
|
gptkbp:services
|
gptkb:Soyuz_service_module
|
|
gptkbp:successor
|
gptkb:Soyuz_7K-OKS
|
|
gptkbp:usedIn
|
gptkb:Salyut_program
Almaz_program
|