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gptkbp:instance_of
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gptkb:spacecraft
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gptkbp:collaboration
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ESA participation
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gptkbp:communication_system
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gptkb:radio_station
|
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gptkbp:control_system
|
automatic and manual
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|
gptkbp:cooling_system
|
phenolic resin
ablative heat shield
|
|
gptkbp:crew
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gptkb:Alexander_Kaleri
gptkb:Yuri_Baturin
gptkb:Thomas_Reiter
gptkb:launch_escape_system
extensive pre-flight training
safe return to Earth
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|
gptkbp:crew_capacity
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gptkb:3
|
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gptkbp:date
|
March 2000
|
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gptkbp:diameter
|
2.2 m
|
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gptkbp:first_flight
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gptkb:Soyuz_TM-1
gptkb:Soyuz_TM-31
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gptkbp:historical_significance
|
part of ISS program
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|
https://www.w3.org/2000/01/rdf-schema#label
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Soyuz TM-30 descent module
|
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gptkbp:landing_site
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gptkb:Kazakhstan
2000-03-25
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gptkbp:launch_date
|
1999-04-20
|
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gptkbp:launch_mass
|
7,200 kg
|
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gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz-FG
|
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gptkbp:launch_window
|
April 1999
|
|
gptkbp:launched
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gptkb:Russian_space_agency
|
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gptkbp:legacy
|
contributed to human spaceflight knowledge
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:life_support_system
|
closed-loop system
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mission
|
gptkb:Moscow_Mission_Control_Center
successful
successfully analyzed
|
|
gptkbp:mission_duration
|
10 months
|
|
gptkbp:mission_type
|
manned spaceflight
|
|
gptkbp:module
|
approximately 30 minutes
ballistic descent
|
|
gptkbp:navigation_system
|
inertial navigation
|
|
gptkbp:orbital_period
|
90 minutes
|
|
gptkbp:part_of
|
Soyuz TM-30 mission
|
|
gptkbp:payload_capacity
|
gptkb:scientific_experiments
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:recovery_method
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gptkb:parachute
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:speed
|
28,000 km/h
6.5 degrees
|
|
gptkbp:successor
|
gptkb:Soyuz_TM-31
|
|
gptkbp:weight
|
7,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_TM-30
|
|
gptkbp:bfsLayer
|
6
|