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gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:communication_system
|
S-band radio
|
|
gptkbp:control_system
|
Inertial navigation system
|
|
gptkbp:cooling_system
|
gptkb:Phenolic-impregnated_carbon_ablator
ablative heat shield
|
|
gptkbp:crew
|
gptkb:Oleg_Novitskiy
gptkb:Chris_Cassidy
gptkb:Alexander_Skvortsov
gptkb:launch_escape_system
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:duration
|
180 days
|
|
gptkbp:first_flight
|
gptkb:Soyuz_MS-19
gptkb:Soyuz_TMA-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz TMA-23 descent module
|
|
gptkbp:is_a_destination_for
|
gptkb:International_Space_Station
|
|
gptkbp:landing_distance
|
main and reserve parachutes
|
|
gptkbp:landing_site
|
gptkb:Kazakhstan
July 1, 2013
|
|
gptkbp:launch_date
|
December 19, 2012
|
|
gptkbp:launch_mass
|
7,200 kg
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz-FG
|
|
gptkbp:launched
|
gptkb:Russian_Federal_Space_Agency
|
|
gptkbp:life_support_system
|
closed-loop system
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mass
|
7,200 kg
|
|
gptkbp:mission
|
Soyuz TMA-23 mission patch
|
|
gptkbp:mission_duration
|
5 months
|
|
gptkbp:mission_type
|
gptkb:human_spaceflight
|
|
gptkbp:module
|
ballistic descent
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:orbit_type
|
Low Earth Orbit
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:part_of
|
gptkb:Soyuz_program
|
|
gptkbp:predecessor
|
gptkb:Soyuz_TMA-22
|
|
gptkbp:related_vehicle
|
gptkb:Soyuz_TMA-23
|
|
gptkbp:speed
|
7.5 km/s
|
|
gptkbp:successor
|
gptkb:Soyuz_TMA-24
|
|
gptkbp:team
|
Russian Search and Recovery Forces
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_TMA-23
|
|
gptkbp:bfsLayer
|
6
|