|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:communicationEquipment
|
radio
|
|
gptkbp:controls
|
automated and manual
|
|
gptkbp:crew
|
3
extensive
|
|
gptkbp:crewCapacity
|
3
high safety standards
launch escape system
|
|
gptkbp:decommissioned
|
1971
|
|
gptkbp:design
|
modular design
manned space missions
|
|
gptkbp:diameter
|
2.2 m
|
|
gptkbp:diedIn
|
closed-loop system
|
|
gptkbp:environmentalImpact
|
ablative heat shield
|
|
gptkbp:firstFlight
|
gptkb:Soyuz_11
gptkb:Soyuz_10
1
1971-10-30
first flight of the series
|
|
gptkbp:historicalSignificance
|
pioneering spacecraft design
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz 7K-OKS-3
|
|
gptkbp:influenced
|
later_Soyuz_models
|
|
gptkbp:internationalCooperation
|
used in international missions
|
|
gptkbp:involvedIn
|
gptkb:Salyut_program
|
|
gptkbp:landingGear
|
gptkb:Kazakhstan
|
|
gptkbp:launchDate
|
1971-10-30
|
|
gptkbp:launched
|
successful
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
6800 kg
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz_rocket
|
|
gptkbp:legacy
|
foundation for future spacecraft.
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:manufacturer
|
gptkb:OKB-1
|
|
gptkbp:mission
|
crewed spaceflight
|
|
gptkbp:missions
|
10 days
|
|
gptkbp:navigationEquipment
|
inertial navigation
|
|
gptkbp:notableEvent
|
first flight of the Soyuz 7K-OKS series
|
|
gptkbp:operatedBy
|
gptkb:Soviet_space_program
|
|
gptkbp:operationalStatus
|
1971
retired
|
|
gptkbp:orbitalInclination
|
90 minutes
|
|
gptkbp:payloadCapacity
|
up to 1000 kg
|
|
gptkbp:powers
|
solar panels
|
|
gptkbp:primaryFunction
|
transport to space station
|
|
gptkbp:renovated
|
parachute
|
|
gptkbp:respondsTo
|
gptkb:Soyuz_descent_module
|
|
gptkbp:safetyFeatures
|
high safety record
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Soyuz_program
gptkb:Soyuz_T
|