Soyuz TM series

GPTKB entity

Statements (64)
Predicate Object
gptkbp:instance_of gptkb:spacecraft
gptkbp:collaboration yes
gptkbp:communication_system gptkb:radio_station
gptkbp:cooling_system ablative heat shield
gptkbp:crew gptkb:Valentina_Tereshkova
gptkb:launch_escape_system
yes
required
multiple redundancy
gptkbp:crew_capacity gptkb:3
gptkbp:decommissioned gptkb:2009
gptkbp:design 6 months
gptkbp:designed_by gptkb:Soviet_Union
gptkbp:diameter 2.2 m
gptkbp:durability false
gptkbp:emergency_services possible
gptkbp:first_flight gptkb:1986
gptkb:2009
gptkb:TM-15
gptkb:TM-1
gptkbp:flight_style gptkb:15
gptkbp:historical_significance first spacecraft to regularly transport crew to Mir
https://www.w3.org/2000/01/rdf-schema#label Soyuz TM series
gptkbp:landing_distance gptkb:parachute
gptkbp:launch_date annual
gptkbp:launch_mass 7,200 kg
gptkbp:launch_platform gptkb:Russian_space_agency
gptkbp:launch_price $20 million
gptkbp:launch_site gptkb:Baikonur_Cosmodrome
gptkbp:launch_vehicle gptkb:Soyuz_spacecraft
gptkbp:legacy foundation for future spacecraft designs.
gptkbp:length 7.2 m
gptkbp:life_support_system yes
gptkbp:manufacturer gptkb:RSC_Energia
gptkbp:mass 7,200 kg
gptkbp:mission gptkb:15
gptkb:Moscow
yes
gptkbp:mission_type Low Earth Orbit
gptkbp:navigation_system gptkb:navigation_system
gptkbp:notable_mission Mir missions
gptkbp:objective transport to space station
gptkbp:operational_period 1986-2009
gptkbp:operational_status retired
gptkbp:orbital_inclination 51.6 degrees
gptkbp:orbital_period 90 minutes
gptkbp:payload_capacity 1,000 kg
gptkbp:power_source solar panels
gptkbp:recovery_method yes
gptkbp:reliability high
gptkbp:safety_record high
gptkbp:service yes
1986-2009
gptkbp:spacecraft gptkb:Soyuz
multi-purpose
gptkbp:speed ballistic reentry
gptkbp:successor gptkb:Soyuz_TMA_series
gptkbp:used_for manned spaceflight
gptkbp:bfsParent gptkb:Soyuz_TM-18
gptkb:Soyuz_TM-5
gptkb:Soyuz_87
gptkb:Soyuz_TM-31
gptkb:Soyuz_7_K-OKS
gptkbp:bfsLayer 5