Injection head for rocket engines

Details Injection head for rocket engines Injection head for rocket engines

1997-06-26

1999-11-16

Freay, Charles G.

Power plants

Reaction motor

Liquid oxidizer

239562, F02K 900

Patent

active

059836261

ABSTRACT:
An injection head for rocket engines, in the combustion chambers of which one or more liquid propellants are chemically reacted to generate thrust, with a plurality of injection elements as well as with a distribution chamber arranged before these injection elements in terms of flow. The distribution chamber is divided into two chambers connected in series in terms of flow by means of a separator plate arranged at right angles to the longitudinal direction of the engine. The separator plate has a plurality of openings, each with a different flow cross section and with a defined direction of flow, wherein each opening is associated with one or more injection elements.

REFERENCES:
patent: 3194012 (1965-07-01), Horrocks
patent: 3266241 (1966-08-01), Jennings
patent: 5456065 (1995-10-01), Dargies
patent: 5660039 (1997-08-01), Sion et al.
patent: 5771579 (1998-06-01), Farhangi et al.

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