Abstract: A hinge assembly of a system for operating a door of an aircraft includes a bracket secured to a structure of the aircraft. The bracket includes a first forward joint and a first aft joint separated by a first distance along a first line. A forward link is coupled to the first forward joint. An aft link is longer than the forward link, and is coupled to the first aft joint. A door coupler is secured to a door. The door coupler includes a second forward joint and a second aft joint separated by a second distance that is less than the first distance. The second distance is along a second line that is parallel to the first line in a stowed position. The forward link is further coupled to the second forward joint, and the aft link is further coupled to the second aft joint.

Abstract: A flexible polyurethane foam comprises up to 10 wt % of a fumed silica having a surface area from 50 to 150 m2/g, wherein the fumed silica has C1-C3 alkylsilyl groups at its surface, the flexible polyurethane foam exhibiting has a resilience of at least 40%, for example, from 40% to 70%, a dry compression set no greater than 15%, for example, from 3% to 15%, or both. Alternatively in addition, the flexible polyurethane foam may have a compression force deflection at 50% as measured by ASTM D3574 that is at least 30%, for example, at least 50%, at least 70%, or from 30% to 155%, greater than a flexible polyurethane foam having the same composition but with polyol replacing the silica.

Abstract: A propulsionless munition configured to be launched from a hypersonic aerial includes a munition body that is free of any propulsion system for producing thrust. The munition body includes a forward section including a radome assembly and an aft section including a control system. The radome assembly includes a nose radome and a frangible radome cover disposed over the nose radome for shielding the nose radome from high temperatures resulting from aerodynamic heating at hypersonic speeds. The frangible radome cover is detachable from the nose radome upon detection by the control system of a predetermined threshold comprising at least one of a predetermined speed, a predetermined altitude, and a predetermined temperature.

Abstract: A system and method for ejecting a store from an aircraft include a stowage tube configured to retain the store. The stowage tube includes an open rear end. A door panel is coupled to the stowage tube. An actuator driven linkage is coupled to the door panel. The actuator driven linkage is configured to rotate the door panel about a pivot axis at a forward edge opposite from an aft end between a closed position associated with a stowed position of the system and an open position associated with a deployed position of the system. The stowage tube is configured to rearwardly eject the store out of the open rear end when the system is in the deployed position.

Abstract: A hinge assembly of a system for operating a door of an aircraft includes a bracket secured to a structure of the aircraft. The bracket includes a first forward joint and a first aft joint separated by a first distance. A forward link is coupled to the first forward joint. An aft link is longer than the forward link, and is coupled to the first aft joint. A door coupler is secured to a door. The door coupler includes a second forward joint and a second aft joint separated by a second distance that is less than the first distance. The forward link is further coupled to the second forward joint, and the aft link is further coupled to the second aft joint.

Abstract: A store ejector rack including a first hook member and a second hook member, a split sleeve guide member, and a pair of split sleeve members, including a first split sleeve member and a second split sleeve member, operatively coupled to the split sleeve guide member. The first split sleeve member is coupled to the first hook member and the second split sleeve member is coupled to the second hook member. A valve control assembly is operatively coupled to the split sleeve guide member, wherein actuation of the split sleeve guide member causes actuation of the first hook member, the second hook member, and the valve control assembly.

Abstract: A multiple advanced missile and bomb ejector rack carriage system employs a carriage mountable to an air to ground (AG) bomb release unit (BRU) on an aircraft pylon. A single MIL-STD-1760 electrical interface is integral to the carriage and has a first power connection and first signal connection. Onboard carriage avionics are supported within the carriage and connected to the MIL-STD-1760 electrical interface. The onboard carriage avionics are adapted to receive communications from an aircraft central computer through the first power connection and first signal connection and provide store specific communications independent of specific original aircraft wiring to at least one ejector and store.

Abstract: A store ejector rack including a first hook member and a second hook member, a split sleeve guide member, and a pair of split sleeve members, including a first split sleeve member and a second split sleeve member, operatively coupled to the split sleeve guide member. The first split sleeve member is coupled to the first hook member and the second split sleeve member is coupled to the second hook member. A valve control assembly is operatively coupled to the split sleeve guide member, wherein actuation of the split sleeve guide member causes actuation of the first hook member, the second hook member, and the valve control assembly.

Abstract: A multiple advanced missile and bomb ejector rack carriage system employs a carriage mountable to an air to ground (AG) bomb release unit (BRU) on an aircraft pylon. A single MIL-STD-1760 electrical interface is integral to the carriage and has a first power connection and first signal connection. Onboard carriage avionics are supported within the carriage and connected to the MIL-STD-1760 electrical interface. The onboard carriage avionics are adapted to receive communications from an aircraft central computer through the first power connection and first signal connection and provide store specific communications independent of specific original aircraft wiring to at least one ejector and store.

Abstract: A package assembly includes a panel, an array of openings defined in the panel, and a plurality of syringe wells. The panel includes an upper surface. Each of the syringe wells is individually associated with a different one of the openings. The panel and the plurality of syringe wells are integrally formed as a unitary structure. Each of the syringe wells is configured to removeably receive a syringe assembly.

Abstract: In one embodiment there is provided a radar signature and induced aerodynamic drag minimizing, externally mountable, internally configurable pod structure optimized for internal placement of one or more deployable stores through configuration and optimal kinematic operation of a pod door assembly. The pod structure has an externally mountable pod housing, a predetermined pod housing cross-sectional configuration optimized to provide a configurable interior volume accommodating multiple different store configurations, and a predetermined pod housing configuration having a cross-sectional configuration optimized to minimize a radar signature and an induced aerodynamic drag. The pod structure further has a pod door assembly integral with the pod housing and having a plurality of pod doors and one or more seal door mechanism assemblies. The pod structure is optimized in kinematic operational combination of the pod doors and seal door mechanism assemblies controlling ejection launch envelopes.

Abstract: A package assembly includes a panel, an array of openings defined in the panel, and a plurality of syringe wells. The panel includes an upper surface, Each of the syringe wells is individually associated with a different one of the openings. The panel and the plurality of syringe wells are integrally formed as a unitary structure. Each of the syringe wells is configured to removeably receive a syringe assembly.

Abstract: A package assembly includes a plurality of syringe assemblies. Each syringe assembly has a syringe flange defining an opening. The syringe flange of each of the syringe assemblies is coupled to a plurality of adjacent syringe flanges to define a panel. Each of the syringe flanges includes a plurality of lateral edges. The plurality of lateral edges of each syringe flange is coupled to the lateral edge of adjacent syringe flanges in a breakaway configuration to facilitate separation of each of the plurality of syringe assemblies from the panel.

Abstract: In one embodiment there is provided a radar signature and induced aerodynamic drag minimizing, externally mountable, internally configurable pod structure optimized for internal placement of one or more deployable stores through configuration and optimal kinematic operation of a pod door assembly. The pod structure has an externally mountable pod housing, a predetermined pod housing cross-sectional configuration optimized to provide a configurable interior volume accommodating multiple different store configurations, and a predetermined pod housing configuration having a cross-sectional configuration optimized to minimize a radar signature and an induced aerodynamic drag. The pod structure further has a pod door assembly integral with the pod housing and having a plurality of pod doors and one or more seal door mechanism assemblies. The pod structure is optimized in kinematic operational combination of the pod doors and seal door mechanism assemblies controlling ejection launch envelopes.

Abstract: A package assembly includes a panel, an array of openings defined in the panel, and a plurality of syringe wells. The panel includes an upper surface. Each of the syringe wells is individually associated with a different one of the openings. The panel and the plurality of syringe wells are integrally formed as a unitary structure. Each of the syringe wells is configured to removeably receive a syringe assembly.

Abstract: A package assembly includes a panel, an array of openings defined in the panel, and a plurality of syringe wells. The panel includes an upper surface. Each of the syringe wells is individually associated with a different one of the openings. The panel and the plurality of syringe wells are integrally formed as a unitary structure. Each of the syringe wells is configured to removeably receive a syringe assembly.

Abstract: A package assembly includes a panel, an array of openings defined in the panel, and a plurality of syringe wells. The panel includes an upper surface. Each of the syringe wells is individually associated with a different one of the openings. The panel and the plurality of syringe wells are integrally formed as a unitary structure. Each of the syringe wells is configured to removeably receive a syringe assembly.

Abstract: A syringe assembly includes a syringe body including a distal end. The syringe body defines a fluid chamber therein. The fluid chamber includes a lower end. A septum is disposed at the distal end of the syringe body and is configured to sealingly close the lower end of the fluid chamber. The syringe body and the septum are formed as a single, molded piece.

Abstract: The present disclosure relates to a vial transfer needle assembly including a first molding member and a second molding member. The first molding member includes a hub portion that has a proximal piercing tip and a distal portion. The hub portion defines a lumen that passes therethrough. The second molding member includes a central housing, a proximal skirt, and a distal skirt. The second molding portion is molded at least partially about the first molding portion to form a monolithic structure. The piercing tip is positioned to extend into a first cavity that is defined by the proximal skirt. The distal portion of the first molding member is positioned to extend through a second cavity that is defined by the skirt. The distal skirt is dimensioned to receive a medical device.

Abstract: The present disclosure relates to a vial transfer needle assembly that includes a housing and a vial access member. The housing includes a proximal skirt and a distal skirt that is connected by a central hub portion. The central hub portion defines a central bore that extends between the proximal skirt and the distal skirt. The central bore of the housing includes an annular bead, a side wall, and a shoulder. The vial access member is disposed within the central bore of the housing such that the top surface of the flange is positioned underneath the annular bead of the central bore to thereby secure the vial access member within the housing.