|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:communication
|
radio and telemetry
|
|
gptkbp:control_system
|
automatic and manual
|
|
gptkbp:cooling_system
|
gptkb:shield
|
|
gptkbp:crew
|
gptkb:Georgi_Shonin
gptkb:Viktor_Patsayev
gptkb:Valentin_Lebedev
gptkb:launch_escape_system
1971-03-07
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:decommissioned
|
gptkb:1971
|
|
gptkbp:design_purpose
|
transport crew to space station
|
|
gptkbp:diameter
|
2.2 m
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
|
|
gptkbp:first_flight
|
1971-03-02
|
|
gptkbp:flight_style
|
gptkb:1
|
|
gptkbp:fuel_type
|
hypergolic propellant
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz 7 K-OKS-14
|
|
gptkbp:landing_site
|
gptkb:Kazakhstan
1971-03-07
|
|
gptkbp:launch_date
|
1971-03-02
|
|
gptkbp:launch_event
|
successful
|
|
gptkbp:launch_mass
|
6800 kg
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:life_support_system
|
environmental control system
|
|
gptkbp:manufacturer
|
gptkb:OKB-1
|
|
gptkbp:mass
|
6800 kg
|
|
gptkbp:mission
|
gptkb:Soyuz_10
successful
|
|
gptkbp:mission_duration
|
5 days
|
|
gptkbp:mission_type
|
gptkb:human_spaceflight
|
|
gptkbp:navigation_system
|
gptkb:navigation_system
|
|
gptkbp:next_edition
|
gptkb:Soyuz_7_K-OKS-13
gptkb:Soyuz_7_K-OKS-15
|
|
gptkbp:operational_period
|
gptkb:1971
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:orbital_altitude
|
200 km
low Earth orbit
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:payload_capacity
|
1000 kg
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:related_vehicle
|
gptkb:Soyuz_descent_module
|
|
gptkbp:speed
|
28,000 km/h
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Soyuz_program
gptkb:Soyuz_T
|
|
gptkbp:bfsParent
|
gptkb:Roscosmos
|
|
gptkbp:bfsLayer
|
4
|