Injection head for rocket engines
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United States of America Patent
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Nov 16, 1999
Grant Date -
N/A
app pub date -
Jun 26, 1997
filing date -
Jun 27, 1996
priority date (Note) -
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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.
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