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gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:communicationEquipment
|
radio communication
|
|
gptkbp:controls
|
automated and manual
|
|
gptkbp:crew
|
gptkb:Oleg_Makarov
gptkb:Viktor_Patsayev
Cosmonaut training program
Valentin Lebedev
|
|
gptkbp:crewCapacity
|
3
|
|
gptkbp:designedBy
|
gptkb:Soviet_Union
|
|
gptkbp:diameter
|
2.2 m
|
|
gptkbp:diedIn
|
environmental control system
|
|
gptkbp:firstFlight
|
gptkb:Soyuz_10
gptkb:Soyuz_12
1970-04-03
1971-10-30
|
|
gptkbp:historicalSignificance
|
first spacecraft to dock with space station
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz 7K-LOK
|
|
gptkbp:influenced
|
future_Soyuz_designs
|
|
gptkbp:influencedBy
|
gptkb:Vostok_program
|
|
gptkbp:landingGear
|
parachute system
|
|
gptkbp:launchDate
|
1970-04-03
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
6800 kg
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz_rocket
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:manufacturer
|
gptkb:OKB-1
|
|
gptkbp:mission
|
low_Earth_orbit
|
|
gptkbp:missions
|
gptkb:Moscow_Mission_Control
up to 10 days
|
|
gptkbp:notableFeature
|
modular design
advanced navigation systems
crew safety measures
versatile mission capabilities
reliable launch system
|
|
gptkbp:numberOfFigures
|
3
|
|
gptkbp:operationalStatus
|
1970-1971
|
|
gptkbp:orbitalInclination
|
200-300 km
28,000 km/h
|
|
gptkbp:payloadCapacity
|
up to 300 kg
|
|
gptkbp:powers
|
solar panels
|
|
gptkbp:propulsion
|
liquid fuel engines
|
|
gptkbp:purpose
|
manned space missions
|
|
gptkbp:replacedBy
|
gptkb:Soyuz_T
|
|
gptkbp:respondsTo
|
heat shield
|
|
gptkbp:secondaryMission
|
1971-10-30
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Soyuz_7K-OK
|