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gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:air_traffic_control
|
onboard computer system
|
|
gptkbp:aircraft_operated
|
varies by mission
over 150 crewed flights
|
|
gptkbp:capacity
|
3 crew members
|
|
gptkbp:communication_system
|
gptkb:radio_station
|
|
gptkbp:control_surfaces
|
reaction control thrusters
|
|
gptkbp:control_system
|
automatic and manual
|
|
gptkbp:cooling_system
|
thermal insulation
ablative material
|
|
gptkbp:crew
|
gptkb:launch_escape_system
extensive training required
multiple safety systems in place
experienced astronauts preferred
returns crew from ISS
|
|
gptkbp:current_use
|
International Space Station missions
|
|
gptkbp:design
|
approximately 6 months
|
|
gptkbp:design_features
|
conical shape
|
|
gptkbp:designed_by
|
gptkb:S._P._Korolev_Rocket_and_Space_Corporation_Energia
|
|
gptkbp:dimensions
|
2.2 meters in diameter
|
|
gptkbp:emergency_services
|
controlled descent
|
|
gptkbp:first_flight
|
gptkb:Soyuz_1
|
|
gptkbp:historical_significance
|
first crewed spacecraft to return safely from space
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz Descent Module
|
|
gptkbp:landing_distance
|
gptkb:parachute
at 10,000 feet
|
|
gptkbp:launch_date
|
gptkb:1967
multiple launches per year
|
|
gptkbp:launch_platform
|
gptkb:missions
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:life_support_system
|
environmental control system
|
|
gptkbp:mass
|
approximately 2,500 kg
|
|
gptkbp:modifications
|
various upgrades over the years
|
|
gptkbp:navigation_system
|
gptkb:navigation_system
|
|
gptkbp:operational_since
|
gptkb:1967
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:operational_use
|
ground control and onboard crew
|
|
gptkbp:origin
|
gptkb:Soviet_space_program
|
|
gptkbp:part_of
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:payload_capacity
|
limited to crew and small cargo
|
|
gptkbp:post_landing
|
subject to inspection and refurbishment
|
|
gptkbp:recovery_method
|
land or water
parachute and soft landing
|
|
gptkbp:related_vehicle
|
gptkb:Mi-8_helicopter
|
|
gptkbp:safety_record
|
high safety record
|
|
gptkbp:seating_capacity
|
crew ejection seat
|
|
gptkbp:service
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:specification
|
detailed engineering documents available.
|
|
gptkbp:speed
|
up to 7.9 km/s
approximately 6 degrees
|
|
gptkbp:successor
|
gptkb:Soyuz_MS_series
|
|
gptkbp:team
|
search and rescue team
|
|
gptkbp:used_by
|
gptkb:Russian_space_program
|
|
gptkbp:used_for
|
crew return
|
|
gptkbp:user_countries
|
used by multiple countries
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_TMA-12_M
gptkb:Soyuz_TMA-16_M
gptkb:Soyuz_TMA-6
gptkb:Soyuz_MS-29
gptkb:Soyuz_MS-72
gptkb:Soyuz_MS-76
gptkb:Soyuz_MS-78
gptkb:Soyuz_TMA-11_M
|
|
gptkbp:bfsLayer
|
5
|