|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:air_traffic_control
|
automatic and manual control
|
|
gptkbp:communication_system
|
S-band
|
|
gptkbp:control_system
|
KURS-NA
|
|
gptkbp:cooling_system
|
phenolic resin
ablative heat shield
|
|
gptkbp:crew
|
gptkb:Alexander_Gerst
gptkb:Andrey_Babkin
gptkb:Shane_Kimbrough
gptkb:launch_escape_system
safe return to Earth
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:dimensions
|
2.2 m diameter
|
|
gptkbp:first_flight
|
gptkb:2016
gptkb:2017
|
|
gptkbp:has_authority_over
|
gptkb:Russian_Federal_Space_Agency
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz MS-03 descent module
|
|
gptkbp:landing_distance
|
three main parachutes
|
|
gptkbp:landing_site
|
gptkb:Kazakhstan
2017-04-10
|
|
gptkbp:launch_date
|
2016-11-17
|
|
gptkbp:launch_mass
|
9,500 kg
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz-FG
|
|
gptkbp:launched
|
gptkb:Soyuz-FG_rocket
|
|
gptkbp:life_support_system
|
closed-loop system
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mission
|
ISS resupply
|
|
gptkbp:mission_duration
|
173 days
|
|
gptkbp:mission_type
|
gptkb:human_spaceflight
|
|
gptkbp:module
|
ballistic descent
part of Soyuz spacecraft
|
|
gptkbp:navigation_system
|
gptkb:navigation_system
|
|
gptkbp:operational_history
|
part of ISS program
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:part_of
|
Soyuz MS-03 mission
|
|
gptkbp:payload_capacity
|
gptkb:scientific_experiments
|
|
gptkbp:recovery_method
|
helicopter and ground teams
|
|
gptkbp:speed
|
7.5 km/s
|
|
gptkbp:status
|
successfully completed mission
|
|
gptkbp:successor
|
gptkb:Soyuz_MS-04
|
|
gptkbp:team
|
gptkb:Kazakhstan_recovery_forces
|
|
gptkbp:weight
|
7,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_MS-03
|
|
gptkbp:bfsLayer
|
5
|