An exhaust system has an engine exhaust plane associated with an entrance to the exhaust system, an exhaust exit plane associated with an exit of the exhaust system, a forward cap movable relative to the engine exhaust plane and configured to selectively intersect the engine exhaust plane, and an aft cap movable relative to the exhaust exit plane and configured to selectively intersect the exhaust exit plane.
Adaptive engine exhaust signature suppressor
2019-10-29
Patent
Electronic Resource
English
Rapid Response Flight Test on MH-47G Engine Exhaust Suppressor
British Library Conference Proceedings | 2011
|NTIS | 1974
|NTRS | 1974
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