Integrated airbreathing and non-airbreathing engine system
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United States of America Patent
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May 25, 2010
Grant Date -
Nov 19, 2009
app pub date -
Feb 15, 2006
filing date -
Feb 15, 2006
priority date (Note) -
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Abstract
An engine assembly includes a gas-turbine engine having a tailcone portion and a bypass duct, a rocket engine combustion assembly located at the tailcone portion of the gas-turbine engine, and a movable nozzle segment subassembly that is selectively engageable with the gas-turbine engine bypass duct in an open position and with the rocket engine combustion assembly in a closed position.
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