combustionChamberDesign
P92045
predicate
Indicates the specific configuration and structural characteristics of a combustion chamber that determine how fuel and oxidizer mix, ignite, and burn within an engine or reactor.
Observed surface forms (3)
| Surface form | Occurrences |
|---|---|
| combustionChamberArrangement | 4 |
| combustionChamberFeature | 2 |
| combustorGeometry | 1 |
Sample triples (8)
| Subject | Object |
|---|---|
| Vortec V6 | Vortec-style high-swirl ⓘ |
| RD-180 | two side-by-side chambers with a common turbopump via predicate surface "combustionChamberArrangement" ⓘ |
| RD-191 | single-chamber version of RD-170 family via predicate surface "combustionChamberArrangement" ⓘ |
| 3.0-liter twin-turbocharged V6 Nettuno | pre-chamber with spark plug via predicate surface "combustionChamberFeature" ⓘ |
| 3.0-liter twin-turbocharged V6 Nettuno | lateral spark plug in main chamber via predicate surface "combustionChamberFeature" ⓘ |
| TAPS (Twin Annular Pre-mixing Swirler) | annular combustor via predicate surface "combustorGeometry" ⓘ |
| RD-171 | clustered around central turbopump via predicate surface "combustionChamberArrangement" ⓘ |
|
RD-191 rocket engine
surface form:
RD-191
|
single-chamber via predicate surface "combustionChamberArrangement" ⓘ |