System and method for independent retention and release of individually stowed flight control surfaces
作者： Copp James C , Ellzey Steven J
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摘要: An aircraft is provided comprising: a fuselage, first tail fin rotatably mounted to lateral side and second the side. A wing body underside of fuselage. pair independent latch release devices are independently when having angle in stowed position with respect unlatch response third The angle, different angles longitudinal axis
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