Properties (56)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
Engine
|
| gptkbp:canBe |
Horizontal
Vertical Reusable Cryogenic Multi-stage Single-stage Liquid-fueled Solid-fueled |
| gptkbp:hasEvents |
High Efficiency
|
| gptkbp:hasType |
Hybrid
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rocket Engine
|
| gptkbp:isAttendedBy |
Gravity
|
| gptkbp:isCriticizedFor |
Spacecraft_Propulsion
|
| gptkbp:isDesignedFor |
Specific Missions
Minimize Weight |
| gptkbp:isEvaluatedBy |
Performance Metrics
Thrust-to-Weight Ratio Specific Impulse |
| gptkbp:isInfluencedBy |
Aerodynamics
|
| gptkbp:isPartOf |
gptkb:Space_Launch_System
Launch Vehicle Launch Pad Setup Propulsion_Technology Rocket_Design Rocket_Propulsion_System |
| gptkbp:isSubjectTo |
Regulations
Environmental Regulations Thermal Stress |
| gptkbp:isTestedFor |
Reliability
Safety Standards Performance Under Load Test Facilities |
| gptkbp:isTrainedIn |
Static Fire Tests
|
| gptkbp:isUsedFor |
Manned Missions
Unmanned Missions |
| gptkbp:isUsedIn |
Space Exploration
Space Shuttle Military Applications Commercial Launches Interplanetary_Missions Orbital_Launches Satellite_Launch NASA_Artemis SpaceX_Falcon |
| gptkbp:isVisitedBy |
gptkb:SpaceX
Blue Origin Computer Simulations NASA Aerospace Companies Specific Payloads |
| gptkbp:operatesIn |
Propellant
|
| gptkbp:produces |
Thrust
|
| gptkbp:requires |
Fuel Tank
Oxidizer |
| gptkbp:usedIn |
Rocket
|