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gptkbp:instance_of
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gptkb:spacecraft
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gptkbp:air_traffic_control
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Automatic and manual
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gptkbp:collaboration
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gptkb:Soviet_space_program
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gptkbp:communication_system
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VHF/ UHF
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|
gptkbp:crew
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gptkb:3
gptkb:Viktor_Patsayev
gptkb:Valery_Bykovsky
gptkb:Alexander_Serebrov
Cosmonaut training program
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gptkbp:crew_capacity
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gptkb:3
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gptkbp:diameter
|
2.7 m
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gptkbp:emergency_services
|
Abort system
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gptkbp:engine_type
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gptkb:RD-107
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gptkbp:first_flight
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gptkb:Soyuz_1
gptkb:Soyuz_7
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gptkbp:flight_style
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gptkb:1
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gptkbp:fuel_type
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Kerosene and liquid oxygen
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gptkbp:height
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7.3 m
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|
gptkbp:historical_significance
|
First spacecraft to use new technology
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|
https://www.w3.org/2000/01/rdf-schema#label
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Soyuz 45 K-2
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gptkbp:influenced
|
Future Soyuz models
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gptkbp:influenced_by
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gptkb:Soyuz_7_K-OK
|
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gptkbp:landing_site
|
gptkb:Kazakhstan
|
|
gptkbp:launch_date
|
1982-03-27
|
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gptkbp:launch_mass
|
7,200 kg
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz-U
|
|
gptkbp:life_support_system
|
gptkb:Environmental_Protection_Agency
|
|
gptkbp:manufacturer
|
gptkb:Soviet_Union
|
|
gptkbp:mission
|
gptkb:Moscow
successful
|
|
gptkbp:mission_duration
|
7 days
|
|
gptkbp:mission_type
|
manned
|
|
gptkbp:navigation_system
|
Inertial navigation system
|
|
gptkbp:operational_period
|
1982-1983
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:payload_capacity
|
7,000 kg
|
|
gptkbp:powers
|
1,000 W
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:replaced_by
|
gptkb:Soyuz_TM
|
|
gptkbp:safety_features
|
Parachute system
|
|
gptkbp:speed
|
Heat shield
|
|
gptkbp:status
|
retired
|
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gptkbp:successor
|
gptkb:Soyuz_T-10
|