Statements (63)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:spacecraft
|
| gptkbp:air_traffic_control |
ground control operations
|
| gptkbp:aircraft_operated |
approximately 6 months in orbit
|
| gptkbp:collaboration |
NASA and Roscosmos
|
| gptkbp:communication_system |
S-band and UHF
|
| gptkbp:cooling_system |
phenolic resin
ablative heat shield |
| gptkbp:crew |
gptkb:3
gptkb:launch_escape_system extensive pre-flight training returning astronauts to Earth experienced astronauts on board designed with crew safety as a priority |
| gptkbp:crew_capacity |
gptkb:3
|
| gptkbp:descent_control |
controlled descent using thrusters
|
| gptkbp:descent_module_weight |
approximately 2,500 kg
|
| gptkbp:design_features |
modular design for easy assembly
|
| gptkbp:emergency_services |
detailed emergency protocols
|
| gptkbp:first_flight |
gptkb:2023
TBD |
| gptkbp:historical_significance |
part of ISS crew rotation
|
| gptkbp:homeworld |
Earth's surface
|
| https://www.w3.org/2000/01/rdf-schema#label |
Soyuz MS-27 descent module
|
| gptkbp:landing_distance |
three main parachutes
crew extraction and medical checks |
| gptkbp:landing_site |
gptkb:Kazakhstan
2023-09-04 |
| gptkbp:launch_date |
2023-02-20
|
| gptkbp:launch_mass |
approximately 7,200 kg
|
| gptkbp:launch_platform |
controlled from Baikonur Cosmodrome
|
| gptkbp:launch_site |
gptkb:Baikonur_Cosmodrome
|
| gptkbp:launch_vehicle |
gptkb:Soyuz-2.1b
|
| gptkbp:launch_window |
specific launch windows based on ISS orbit
|
| gptkbp:launched |
gptkb:Soyuz-2.1b_rocket
extensive pre-launch preparations |
| gptkbp:life_support_system |
closed-loop life support
|
| gptkbp:manufacturer |
gptkb:RSC_Energia
|
| gptkbp:mission |
data collection and analysis
planned for future ISS missions support ISS operations and research |
| gptkbp:mission_duration |
approximately 6 months
|
| gptkbp:mission_type |
gptkb:human_spaceflight
|
| gptkbp:module |
approximately 3 hours
ballistic descent |
| gptkbp:navigation_system |
gptkb:navigation_system
|
| gptkbp:operational_history |
part of the Soyuz program since 1967
|
| gptkbp:operational_status |
active
|
| gptkbp:orbital_altitude |
approximately 400 km
|
| gptkbp:orbital_inclination |
51.6 degrees
|
| gptkbp:part_of |
Soyuz MS-27 mission
|
| gptkbp:payload_capacity |
limited to crew and essential supplies
|
| gptkbp:post_landing_support |
support for crew post-landing.
|
| gptkbp:recovery_method |
coordinated recovery operations post-landing
|
| gptkbp:safety_features |
multiple redundancy systems
|
| gptkbp:safety_measures |
extensive pre-launch safety tests
|
| gptkbp:service |
Soyuz MS-27 service module
|
| gptkbp:specification |
detailed technical specifications available
|
| gptkbp:speed |
approximately 6.5 degrees
approximately 7.5 km/s |
| gptkbp:success_rate |
high success rate in crewed missions
|
| gptkbp:team |
Russian recovery team
|
| gptkbp:bfsParent |
gptkb:Soyuz_MS-27
|
| gptkbp:bfsLayer |
5
|