Soyuz MS-42 descent module

GPTKB entity

Statements (50)
Predicate Object
gptkbp:instance_of gptkb:spacecraft
gptkbp:air_traffic_control manual and automatic modes
gptkbp:collaboration gptkb:International_Space_Station
gptkbp:communication_system solar panels
S-band and UHF
gptkbp:control_system fly-by-wire system
gptkbp:cooling_system ablative heat shield
gptkbp:crew 3 astronauts
ejection seats
extensive training required
safe return of astronauts
gptkbp:crew_capacity gptkb:3
gptkbp:design Soyuz spacecraft design
gptkbp:diameter 2.2 m
gptkbp:emergency_services gptkb:launch_escape_system
gptkbp:first_flight gptkb:Soyuz_1
gptkbp:fuel_type hypergolic propellant
gptkbp:historical_significance part of human spaceflight history
https://www.w3.org/2000/01/rdf-schema#label Soyuz MS-42 descent module
gptkbp:landing_site 2023-09-01
gptkbp:launch_date 2023-03-01
gptkbp:launch_event over 90%
gptkbp:launch_mass approximately 7,200 kg
gptkbp:launch_site gptkb:Baikonur_Cosmodrome
gptkbp:launch_vehicle gptkb:Soyuz-2.1b
gptkbp:launch_window gptkb:2023
gptkbp:launched gptkb:Russian_space_agency
gptkbp:length 7.2 m
gptkbp:life_support_system closed-loop system
gptkbp:manufacturer gptkb:RSC_Energia
gptkbp:mission data collected for future missions
gptkbp:mission_duration approximately 6 months
gptkbp:mission_type gptkb:human_spaceflight
gptkbp:module controlled descent
gptkbp:navigation_system gptkb:navigation_system
gptkbp:operational_since gptkb:1967
gptkbp:operational_status active
gptkbp:orbital_inclination 51.6 degrees
gptkbp:part_of Soyuz MS-42 mission
gptkbp:payload_capacity gptkb:scientific_experiments
gptkbp:recovery_method gptkb:Kazakhstan
parachute landing
gptkbp:safety_record high safety record
gptkbp:service Soyuz MS-42 service module
gptkbp:speed approximately 7.5 km/s
gptkbp:successor gptkb:Soyuz_MS-43_descent_module
gptkbp:used_for transporting astronauts
gptkbp:weight 7,200 kg
gptkbp:bfsParent gptkb:Soyuz_MS-42
gptkbp:bfsLayer 5