Properties (49)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
Engine
|
| gptkbp:hasContent |
Higher efficiency
Complexity of storage Higher thrust-to-weight ratio Requires insulation |
| gptkbp:hasType |
Liquid rocket engine
Hybrid rocket engine |
| https://www.w3.org/2000/01/rdf-schema#label |
Cryogenic Engines
|
| gptkbp:isAssociatedWith |
gptkb:European_Space_Agency
gptkb:International_Space_Station gptkb:NASA's_Space_Launch_System Space exploration Commercial spaceflight |
| gptkbp:isCharacterizedBy |
High reliability
High performance Low emissions Long burn times Cryogenic_temperatures |
| gptkbp:isPartOf |
Satellites
Launch vehicles Interplanetary missions |
| gptkbp:isRegulatedBy |
gptkb:European_Union_Aviation_Safety_Agency
gptkb:Federal_Aviation_Administration gptkb:National_Aeronautics_and_Space_Administration |
| gptkbp:isStudiedIn |
Aerospace engineering
Fluid dynamics Mechanical engineering Thermodynamics Propulsion systems |
| gptkbp:isTrainedIn |
gptkb:Northrop_Grumman
Rocketdyne Aerojet Rocketdyne |
| gptkbp:isUsedIn |
gptkb:Saturn_V
gptkb:Falcon_9 gptkb:Artemis_program Space Shuttle Lunar missions Mars_missions Spacecraft_propulsion |
| gptkbp:isVisitedBy |
gptkb:SpaceX
Blue Origin NASA Reusable launch systems Deep space exploration Earth-to-orbit_launches |
| gptkbp:operates |
Low temperatures
|
| gptkbp:uses |
Liquid oxygen
Liquid hydrogen Cryogenic_fluids |