Abstract: In a servoactuator system for an aircraft, a strapdown series servoactuator having an external linkage assembly is coupled between the pilot's control stick and a control surface member. The external linkage assembly includes a differential link and servo link having specially tapered stop surfaces adapted to be varied in dimensions to accommodate a wide variety of installations, which stop surfaces cooperate with fixed stops on the servoactuator housing whereby to provide a variety of pilot authority limits and series servo authority limits depending upon particular installation requirements.

Abstract: A flare release system in which a plurality of flares are sequentially lahed from a submerged float. Launching apparatus for each flare comprises a compressed gas cylinder which is ruptured by a firing pin propelled by an electrically initiated squib. Compressed gas escaping from the cylinder powers an ejection piston to force a flare from the submerged float. An electric circuit distributes firing pulses to each flare launching mechanism according to a predetermined sequence.

Abstract: An actuation mine simulator system which enables realistic training experce in mine sweeping operations without the danger accompanying use of live mines. The actuation mine simulator is preprogrammed to respond at predetermined time intervals to actuation by large objects such as ships. The mine simulator includes buoyant flares for signaling actuation, a tethered float having a signal beacon for facilitating recovery, and an underwater acoustic transmitter for locating the simulator at the conclusion of training exercises.