A feasibility study on using inkjet technology, micropumps, and MEMs as fuel injectors for bipropellant rocket engines
Control over drop size distributions, injection rates, and geometrical distribution of fuel and oxidizer sprays in bi-propellant rocket engines has the potential to produce more efficient, more stable, less polluting rocket engines. This control also offers the potential of an engine that can be thr...
| Main Authors: | , , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
2010-07.
|
| Subjects: | |
| Online Access: | Get fulltext |