Statements (57)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:spacecraft
|
| gptkbp:designedFor |
Reentry_into_Earth's_atmosphere
|
| gptkbp:features |
Heat shield
Stabilization system Parachute system |
| gptkbp:firstHeld |
gptkb:Apollo_program
gptkb:Soyuz_program gptkb:Gemini_program |
| gptkbp:hasHistory |
Used in multiple space missions
|
| gptkbp:hasVariants |
Crewed variants
Uncrewed variants |
| https://www.w3.org/2000/01/rdf-schema#label |
Reentry Capsule
|
| gptkbp:isAssociatedWith |
Scientific research
Space exploration Technological advancement |
| gptkbp:isCriticizedFor |
Sample return missions
Safe return of astronauts |
| gptkbp:isDesignedFor |
Splashdown
Controlled descent Landing on solid ground |
| gptkbp:isEquippedWith |
Communication systems
Life support systems Navigation_systems |
| gptkbp:isEvaluatedBy |
Performance metrics
Safety assessments Mission success criteria |
| gptkbp:isInfluencedBy |
Atmospheric conditions
Weight of payload Orbital_trajectory |
| gptkbp:isMonitoredBy |
Telemetry systems
Ground control teams |
| gptkbp:isPartOf |
Space mission
Robotic missions Human spaceflight missions Commercial spaceflight initiatives Future space exploration missions |
| gptkbp:isRegulatedBy |
International treaties
Space law |
| gptkbp:isSubjectTo |
G-forces during descent
Reentry heating |
| gptkbp:isTestedFor |
Structural integrity
Thermal protection Aerodynamic stability |
| gptkbp:isTrainedIn |
Space agencies
|
| gptkbp:isUsedIn |
gptkb:Mars_sample_return_missions
Lunar missions International_Space_Station_missions |
| gptkbp:isVisitedBy |
gptkb:NASA's_Artemis_program
Various aerospace companies Commercial crew program |
| gptkbp:operatesIn |
Low Earth Orbit
|
| gptkbp:requires |
Launch vehicle
|
| gptkbp:suitableFor |
Carrying cargo
Carrying crew |
| gptkbp:usedBy |
gptkb:ESA
gptkb:Roscosmos NASA |