|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:air_traffic_control
|
automated and manual control
|
|
gptkbp:collaboration
|
involved multiple countries
|
|
gptkbp:communication_system
|
radio communication
|
|
gptkbp:cooling_system
|
included
|
|
gptkbp:crew
|
gptkb:Oleg_Artemyev
gptkb:Andrey_Babkin
gptkb:Alexander_Skvortsov
based on training and experience
ensured by design
required prior to flight
safe and successful
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:descent_angle
|
approximately 30 degrees
|
|
gptkbp:design_features
|
modular design
|
|
gptkbp:dimensions
|
2.2 m diameter
|
|
gptkbp:emergency_services
|
included
|
|
gptkbp:first_flight
|
gptkb:Soyuz_TMA_series
|
|
gptkbp:fuel_type
|
hypergolic propellant
|
|
gptkbp:historical_significance
|
part of ISS program
|
|
gptkbp:homeworld
|
March 16, 2011
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz TMA-3 M descent module
|
|
gptkbp:landing_distance
|
conducted by recovery team
during descent
|
|
gptkbp:landing_site
|
gptkb:Kazakhstan
March 16, 2011
|
|
gptkbp:launch_date
|
December 19, 2010
|
|
gptkbp:launch_event
|
high
|
|
gptkbp:launch_mass
|
approximately 7,200 kg
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz-FG
|
|
gptkbp:launch_window
|
limited to specific dates
|
|
gptkbp:launched
|
gptkb:Russian_Federal_Space_Agency
|
|
gptkbp:legacy
|
contributed to human spaceflight
|
|
gptkbp:life_support_system
|
provided for crew
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mission
|
gptkb:International_Space_Station
conducted by engineers
|
|
gptkbp:mission_duration
|
92 days
|
|
gptkbp:mission_type
|
gptkb:human_spaceflight
|
|
gptkbp:module
|
gptkb:Soyuz_TMA-3_M_orbital_module
approximately 30 minutes
controlled descent
approximately 7.9 km/h
|
|
gptkbp:navigation_system
|
inertial navigation
|
|
gptkbp:operational_history
|
part of multiple missions
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:part_of
|
Soyuz TMA-3 M mission
|
|
gptkbp:payload_capacity
|
samples and experiments
|
|
gptkbp:recovery_method
|
standard procedure
|
|
gptkbp:research
|
conducted during mission
|
|
gptkbp:safety_features
|
multiple redundancy
|
|
gptkbp:service
|
gptkb:Soyuz_TMA-3_M_service_module
|
|
gptkbp:speed
|
performed successfully
|
|
gptkbp:successor
|
gptkb:Soyuz_MS_series
gptkb:Soyuz_TMA-4
|
|
gptkbp:team
|
Russian recovery team
|
|
gptkbp:weight
|
approximately 7,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_TMA-3_M
|
|
gptkbp:bfsLayer
|
6
|