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gptkbp:instance_of
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gptkb:spacecraft
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gptkbp:communication_system
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gptkb:radio_station
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gptkbp:control_system
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gptkb:navigation_system
|
|
gptkbp:cooling_system
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gptkb:shield
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|
gptkbp:crew
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gptkb:Soyuz_capsule
gptkb:Soyuz_spacecraft
gptkb:launch_escape_system
pre-flight training
emergency escape system
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gptkbp:crew_capacity
|
gptkb:3
|
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gptkbp:decommissioned
|
gptkb:1982
|
|
gptkbp:design
|
3 years
|
|
gptkbp:design_purpose
|
transport crew to space
|
|
gptkbp:diameter
|
2.2 m
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gptkbp:first_flight
|
gptkb:Soyuz_10
gptkb:Soyuz_36
1973-04-26
1974-10-30
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gptkbp:flight_style
|
gptkb:10
gptkb:3
|
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gptkbp:height
|
7.2 m
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|
https://www.w3.org/2000/01/rdf-schema#label
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Soyuz 74 K
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gptkbp:landing_distance
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gptkb:parachute
|
|
gptkbp:launch_date
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gptkb:1973
1973-04-26
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gptkbp:launch_mass
|
6800 kg
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz-U
gptkb:Team_Rocket
|
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gptkbp:launched
|
gptkb:10
gptkb:Baikonur_Launch_Complex_1
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:life_support_system
|
environmental control system
|
|
gptkbp:manufacturer
|
gptkb:Soyuz_Design_Bureau
|
|
gptkbp:mission
|
gptkb:10
gptkb:Moscow_Mission_Control_Center
gptkb:Moscow_Mission_Control
|
|
gptkbp:mission_duration
|
up to 30 days
|
|
gptkbp:mission_type
|
manned
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|
gptkbp:operational_period
|
1973-1982
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:orbital_altitude
|
gptkb:Soyuz_spacecraft
200-400 km
28,000 km/h
|
|
gptkbp:payload_capacity
|
250 kg
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:production_location
|
gptkb:Soviet_Union
|
|
gptkbp:propulsion
|
liquid rocket engines
|
|
gptkbp:recovery_method
|
parachute recovery system
|
|
gptkbp:retirement_year
|
gptkb:1982
|
|
gptkbp:service
|
gptkb:Soyuz_service_module
|
|
gptkbp:spacecraft
|
gptkb:spacecraft
|
|
gptkbp:speed
|
gptkb:Soyuz_reentry_module
|
|
gptkbp:success_rate
|
100%
|
|
gptkbp:successor
|
gptkb:Soyuz_T_series
gptkb:Soyuz_T
|
|
gptkbp:weight
|
6800 kg
|
|
gptkbp:width
|
2.2 m
|