Rocket engine
US6915627B2 · kind B2 · utility
4Cited by
12References
12Claims
0Family size
Assignees
Inventor
Key dates
| Filing date | Feb 27, 2003 |
| Grant date | Jul 12, 2005 |
| Priority date | — |
| Expiry date | Feb 27, 2023 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2240/1281
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
The invention concerns a rocket engine wherein the combustion chamber includes at least one first monolithic component made of a thermostructural composite material comprising a porous wall through which the fuel is introduced in the core of the combustion chamber. A small part of the fuel is directed towards the neck for it to be cooled.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.