|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:aircraft_operated
|
up to 6 months
|
|
gptkbp:cargo_capacity
|
500 kg
|
|
gptkbp:collaboration
|
gptkb:JAXA
gptkb:ESA
gptkb:Intercosmos_program
gptkb:NASA
|
|
gptkbp:communication
|
gptkb:radio_station
|
|
gptkbp:communication_system
|
S-band
|
|
gptkbp:control_system
|
automated and manual
|
|
gptkbp:cooling_system
|
ablative heat shield
|
|
gptkbp:crew
|
gptkb:Oleg_Atkov
gptkb:Aleksandr_Skvortsov
gptkb:Vladimir_Dzhanibekov
gptkb:radio_station
gptkb:Yuri_Malyshev
gptkb:Viktor_Patsayev
gptkb:Georgi_Beregovoy
gptkb:Lunar_Module
gptkb:Valentin_Lebedev
gptkb:Vladimir_Shatalov
gptkb:Boris_Volynov
gptkb:Star_City
gptkb:Alexander_Serebrov
6 months
continuous
varied backgrounds
life support systems
ejection seats
prior to launch
based on experience
safely to Earth
ensures safety
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:design_purpose
|
transport astronauts
|
|
gptkbp:designed_by
|
gptkb:Soviet_Union
|
|
gptkbp:diameter
|
2.2 m
|
|
gptkbp:emergency_services
|
gptkb:launch_escape_system
|
|
gptkbp:first_flight
|
gptkb:Soyuz_13
gptkb:1980
gptkb:1983
gptkb:Soyuz_10
2023-04-01
|
|
gptkbp:flight_style
|
gptkb:6
predefined trajectory
|
|
gptkbp:height
|
3.5 meters
|
|
gptkbp:historical_significance
|
first spacecraft to dock with a space station
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz 100 K
|
|
gptkbp:influenced_by
|
gptkb:Apollo_program
|
|
gptkbp:inspiration
|
future spacecraft designs
|
|
gptkbp:is_a_destination_for
|
gptkb:International_Space_Station
|
|
gptkbp:landing_distance
|
gptkb:parachute
|
|
gptkbp:launch_date
|
2023-04-01
monthly
|
|
gptkbp:launch_mass
|
7,200 kg
|
|
gptkbp:launch_platform
|
ground control team
|
|
gptkbp:launch_price
|
$50 million
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz-2.1b
gptkb:Soyuz_spacecraft
|
|
gptkbp:launch_window
|
determined by ISS schedule
|
|
gptkbp:legacy
|
foundation for future Soyuz models
|
|
gptkbp:length
|
7.2 meters
7.2 m
|
|
gptkbp:life_support_system
|
closed-loop system
|
|
gptkbp:manufacturer
|
gptkb:Russian_Space_Agency
gptkb:Korolev_Rocket_and_Space_Corporation
|
|
gptkbp:mission
|
gptkb:Moscow
gptkb:Moscow_Mission_Control_Center
conducted
support ISS operations
|
|
gptkbp:mission_duration
|
up to 6 months
|
|
gptkbp:mission_type
|
crewed
low Earth orbit
|
|
gptkbp:navigation_system
|
inertial navigation
|
|
gptkbp:next_edition
|
gptkb:Soyuz_TMA
|
|
gptkbp:notable_mission
|
gptkb:Salyut_7
|
|
gptkbp:operational_cost
|
$20 million per flight
|
|
gptkbp:operational_period
|
1980-1983
|
|
gptkbp:operational_since
|
gptkb:2023
|
|
gptkbp:orbital_altitude
|
400 kilometers
28,000 km/h
uses thrusters
|
|
gptkbp:payload_capacity
|
1,000 kg to LEO
protects cargo
|
|
gptkbp:post_landing_procedure
|
safety checks
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:purpose
|
manned spaceflight
|
|
gptkbp:recovery_method
|
gptkb:Lunar_Module
|
|
gptkbp:related_vehicle
|
gptkb:capsule
|
|
gptkbp:reliability
|
proven
|
|
gptkbp:replaced_by
|
gptkb:Soyuz_T
|
|
gptkbp:research
|
microgravity research
|
|
gptkbp:safety_record
|
high
|
|
gptkbp:service
|
provides life support
provides propulsion
|
|
gptkbp:spacecraft
|
orbital spacecraft
|
|
gptkbp:speed
|
gptkb:shield
|
|
gptkbp:squadrons
|
white and blue
|
|
gptkbp:status
|
active
retired
|
|
gptkbp:successor
|
gptkb:Soyuz_T
gptkb:Soyuz_MS
|
|
gptkbp:team
|
trained personnel
|
|
gptkbp:training
|
1 year
|
|
gptkbp:width
|
2.5 meters
|