Statements (60)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:spacecraft
|
| gptkbp:air_traffic_control |
advanced flight control systems
|
| gptkbp:collaboration |
used in international missions
involved in international partnerships |
| gptkbp:communication_system |
radio communication
|
| gptkbp:control_system |
automatic and manual
|
| gptkbp:cooling_system |
ablative material
thermal protection system |
| gptkbp:crew |
gptkb:launch_escape_system
extensive training required designed with crew safety in mind requires experienced crew crew health monitoring systems included |
| gptkbp:crew_capacity |
gptkb:3
|
| gptkbp:debut |
extensive launch history documented
|
| gptkbp:designed_by |
gptkb:Russian_Federal_Space_Agency
|
| gptkbp:dimensions |
2.2 m diameter
|
| gptkbp:emergency_services |
capable of emergency landing
|
| gptkbp:first_flight |
gptkb:Soyuz_MS-01
|
| gptkbp:has_been_restored |
gptkb:Earth
|
| gptkbp:historical_significance |
part of long history of Soyuz missions
|
| https://www.w3.org/2000/01/rdf-schema#label |
Soyuz MS reentry module
|
| gptkbp:landing_distance |
gptkb:parachute
post-landing recovery operations at 10,000 m altitude |
| gptkbp:landing_site |
designated landing area
|
| gptkbp:launch_date |
approximately 1-2 per year
|
| gptkbp:launch_site |
gptkb:Baikonur_Cosmodrome
|
| gptkbp:launch_vehicle |
compatible with various launch vehicles
|
| gptkbp:launch_window |
specific launch windows required
|
| gptkbp:launched |
gptkb:Soyuz_launch_vehicle
extensive launch preparation required |
| gptkbp:life_support_system |
life support system included
|
| gptkbp:mission |
planned for future missions
|
| gptkbp:mission_duration |
typically 6 months
part of many historical missions |
| gptkbp:mission_type |
gptkb:human_spaceflight
|
| gptkbp:modifications |
various modifications over time
|
| gptkbp:navigation_system |
gptkb:navigation_system
|
| gptkbp:operates_in |
2024
|
| gptkbp:operational_since |
gptkb:2016
|
| gptkbp:part_of |
gptkb:Soyuz_MS_spacecraft
|
| gptkbp:payload_capacity |
limited payload capacity
can return scientific experiments |
| gptkbp:recovery_method |
recovery operations conducted post-landing
|
| gptkbp:reentry_simulation |
reentry simulations conducted
|
| gptkbp:research |
supports scientific research missions
|
| gptkbp:safety_record |
high safety record
|
| gptkbp:service |
gptkb:Soyuz_MS_service_module
|
| gptkbp:specification |
detailed technical specifications available
|
| gptkbp:speed |
ballistic trajectory
up to 28,000 km/h approximately 6 degrees specific reentry profile followed |
| gptkbp:successor |
gptkb:Soyuz_MS-2
|
| gptkbp:team |
Russian recovery forces
|
| gptkbp:used_for |
reentry to Earth's atmosphere
|
| gptkbp:weight |
approximately 2,500 kg
|
| gptkbp:bfsParent |
gptkb:Soyuz_MS-15
|
| gptkbp:bfsLayer |
5
|