Soyuz TM-26 descent module

GPTKB entity

Statements (60)
Predicate Object
gptkbp:instance_of gptkb:spacecraft
gptkbp:air_traffic_control gptkb:ground
gptkbp:collaboration yes
gptkbp:communication_system S-band
gptkbp:control_system automatic and manual
gptkbp:cooling_system phenolic resin
ablative heat shield
gptkbp:crew gptkb:Kazakhstan
gptkb:Valery_Polyakov
gptkb:Thomas_Reiter
gptkb:Alexander_Serebrov
yes
extensive training
1997-06-02
experienced astronauts
gptkbp:crew_capacity gptkb:3
gptkbp:crew_return_system yes
gptkbp:debut gptkb:Soyuz_MS-19
gptkb:Soyuz_1
gptkbp:diameter 2.2 m
gptkbp:duration 180 days
gptkbp:emergency_services yes
gptkbp:first_flight gptkb:Soyuz_MS-19
gptkb:Soyuz_1
gptkbp:homeworld gptkb:Kazakhstan
https://www.w3.org/2000/01/rdf-schema#label Soyuz TM-26 descent module
gptkbp:is_a_destination_for gptkb:Mir_space_station
gptkbp:landing_distance three main parachutes
ballistic descent
gptkbp:landing_site gptkb:Kazakhstan
1997-06-02
gptkbp:launch_date 1996-12-20
gptkbp:launch_mass 7,200 kg
gptkbp:launch_site gptkb:Baikonur_Cosmodrome
gptkbp:launch_vehicle gptkb:Soyuz-U
gptkbp:launched gptkb:Soyuz_spacecraft
gptkbp:length 7.2 m
gptkbp:life_support_system closed-loop system
gptkbp:manufacturer gptkb:RSC_Energia
gptkbp:mass 7,200 kg
gptkbp:mission gptkb:scientific_research
gptkbp:mission_duration 180 days
gptkbp:mission_type gptkb:human_spaceflight
gptkbp:module 7.9 m/s
ballistic descent profile
gptkbp:navigation_system inertial navigation
gptkbp:operational_period 1996-1997
gptkbp:operational_status retired
gptkbp:orbital_inclination 51.6 degrees
gptkbp:part_of Soyuz TM-26 mission
gptkbp:power_source solar panels
gptkbp:recovery_method helicopter recovery
gptkbp:related_vehicle yes
gptkbp:safety_record high safety record
gptkbp:spacecraft gptkb:spacecraft
three-module design
gptkbp:successor gptkb:Soyuz_TM-27
gptkbp:team Russian recovery forces
gptkbp:bfsParent gptkb:Soyuz_TM-26
gptkbp:bfsLayer 6