Translating cowl inlet with retractable propellant injection struts
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United States of America Patent
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Jun 1, 1993
Issued Date -
N/A
app pub date -
Jan 30, 1992
filing date -
Apr 30, 1990
priority date (Note) -
Expired
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Abstract
The invention is an inlet system for a variable geometry transatmospheric air breathing engine. It incorporates a rotatably translatable cowl provided with a rotating lip used in combination with insertable and propellant injection struts.
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