Statements (55)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
Mechanical Component
|
| gptkbp:component |
Liquid Rocket Engine
Solid Rocket Motor |
| gptkbp:coolingSystem |
Ablative Cooling
Film Cooling Radiative Cooling Regenerative Cooling |
| gptkbp:criticalParameter |
Exit Area
Nozzle Angle Nozzle Expansion Ratio Nozzle Length Nozzle Throat Area |
| gptkbp:designer |
Expansion-Deflection Nozzle
Fixed Nozzle Gimbaled Nozzle Plug Nozzle |
| gptkbp:enables |
Expansion of Gases
Supersonic Flow |
| gptkbp:function |
Directs Exhaust Flow
Produces Thrust |
| gptkbp:hasPart |
Throat
Exit Cone Nozzle Lip |
| https://www.w3.org/2000/01/rdf-schema#label |
Rocket Nozzle
|
| gptkbp:introducedIn |
gptkb:Robert_Goddard
1926 |
| gptkbp:inventedBy |
gptkb:Robert_Goddard
|
| gptkbp:material |
gptkb:ceramics
Graphite Nickel Alloy |
| gptkbp:operatesIn |
High Pressure
High Temperature |
| gptkbp:principle |
Conservation of Momentum
|
| gptkbp:relatedTo |
Chamber Pressure
Exhaust Velocity Expansion Ratio Mach Number Nozzle Efficiency Specific Impulse Thrust Vector Control |
| gptkbp:subjectOf |
gptkb:Fluid_Dynamics
Erosion Thermal Protection Rocket Propulsion Cooling Methods |
| gptkbp:type |
Aerospike Nozzle
Bell Nozzle Convergent-Divergent Nozzle |
| gptkbp:usedBy |
gptkb:satellite
gptkb:Sounding_Rockets Missiles Launch Vehicles |
| gptkbp:usedIn |
Rocket Engine
|
| gptkbp:bfsParent |
gptkb:Super_Mario_Sunshine
|
| gptkbp:bfsLayer |
6
|