| 摘要 |
<p>An engine assembly includes a gas-turbine engine having a tailcone portion (130) and a bypass duct (126), a rocket engine combustion assembly (132, 134) located at the tailcone portion (130) of the gas-turbine engine, and a movable nozzle segment subassembly (102) that is selectively engageable with the gas-turbine engine bypass duct (126) in an open position and with the rocket engine combustion assembly in a closed position.</p> |
