F42B15/34

LOW-OBSERVABLE PROJECTILE
20200166319 · 2020-05-28 ·

A radar-absorbing material projectile system including a projectile with an outer layer of radar-absorbing material (RAM). A carrier or armature is disposed around the projectile, protecting the layer of RAM during the firing sequence. In some embodiments the carrier is a discarding carrier which falls away after firing, rendering the projectile low-observable with regard to radar detection due to the layer of RAM.

Active cooling system for electronics on a missile
10627199 · 2020-04-21 · ·

A vessel (10) containing a fluid (liquid and/or gas) at pressure higher than atmospheric pressure which when evacuated from the vessel (10) lowers the temperature of the vessel and thereby creates a self-generated cold sink capable of absorbing thermal energy to maintain electronics and other temperature sensitive missile components within their operational temperature limits.

Active cooling system for electronics on a missile
10627199 · 2020-04-21 · ·

A vessel (10) containing a fluid (liquid and/or gas) at pressure higher than atmospheric pressure which when evacuated from the vessel (10) lowers the temperature of the vessel and thereby creates a self-generated cold sink capable of absorbing thermal energy to maintain electronics and other temperature sensitive missile components within their operational temperature limits.

ACTUATION DEVICE FOR EJECTING AT LEAST ONE REMOVABLE PART OF A MISSILE, PARTICULARLY A NOSE
20200109929 · 2020-04-09 · ·

An actuation device for ejecting a removable part of a missile includes a pyrotechnic actuator having a pyrotechnic charge configured to generate an overpressure and a piston configured to act on the removable part of the missile, at least one retaining rod, and at least one thermal insulation element configured to thermally insulate at least the pyrotechnic charge. The pyrotechnic actuator is configured to break the retaining rod.

ACTUATION DEVICE FOR EJECTING AT LEAST ONE REMOVABLE PART OF A MISSILE, PARTICULARLY A NOSE
20200109929 · 2020-04-09 · ·

An actuation device for ejecting a removable part of a missile includes a pyrotechnic actuator having a pyrotechnic charge configured to generate an overpressure and a piston configured to act on the removable part of the missile, at least one retaining rod, and at least one thermal insulation element configured to thermally insulate at least the pyrotechnic charge. The pyrotechnic actuator is configured to break the retaining rod.

Variable thickness hollow conformal nose cone

The embodiments relate to a conformal, sometimes referred to as aerodynamic, nose cone, and in particular to a hollow conformal nose cone that is transparent to electromagnetic radiation of a predetermined wavelength, or wavelengths, and that comprises a variable thickness such that the electromagnetic radiation received on an outer surface of the nose cone forms a predetermined beam pattern within the nose cone. Also disclosed are mechanisms for generating such hollow conformal nose cones.

Variable thickness hollow conformal nose cone

The embodiments relate to a conformal, sometimes referred to as aerodynamic, nose cone, and in particular to a hollow conformal nose cone that is transparent to electromagnetic radiation of a predetermined wavelength, or wavelengths, and that comprises a variable thickness such that the electromagnetic radiation received on an outer surface of the nose cone forms a predetermined beam pattern within the nose cone. Also disclosed are mechanisms for generating such hollow conformal nose cones.

Advanced cooling system using throttled internal cooling passage flow for a window assembly, and methods of fabrication and use thereof

A window assembly heat transfer system is disclosed in which a window member has a selected transparency to monitored or sensed light wavelengths. One or more passages are provided in the window member for flowing a single-phase or two-phase heat transfer fluid, the passages being optically non-transparent to the monitored or sensed light wavelengths. A mechanism allows either evaporation or condensation of the fluid and/or balancing of a flow of the fluid within the passages. In one embodiment, the window assembly can be made by producing passages in a top surface of a first single plate, optionally producing passages in a bottom surface of a second single plate and bonding the top surface of the first plate to a bottom surface of a second single plate to form the window member with the passage or passages. In another embodiment, the window assembly can be made by providing a core around which the window member material is grown and thereafter removing the core to produce the passage or passages.

Advanced cooling system using throttled internal cooling passage flow for a window assembly, and methods of fabrication and use thereof

A window assembly heat transfer system is disclosed in which a window member has a selected transparency to monitored or sensed electromagnetic wavelengths. One or more passages are provided in the window member for flowing a single-phase or two-phase heat transfer fluid. A mechanism allows either evaporation or condensation of the fluid and/or balancing of a flow of the fluid within the passages. In one embodiment, the window assembly can be made by producing passages in a top surface of a first single plate, optionally producing passages in a bottom surface of a second single plate and bonding the top surface of the first plate to a bottom surface of a second single plate to form the window member with the passage or passages. In another embodiment, the window assembly can be made by providing a core around which the window member material is grown and thereafter removing the core to produce the passage or passages.

Weapon active hazard mitigation method

A mitigation control system, for performing an active hazard mitigation method, is arranged in an environment containing an energetic material and includes an abnormal temperature sensor for detecting an abnormal temperature of the environment, a power source that is mechanically actuated by the abnormal temperature sensor when the abnormal temperature exceeds a predetermined abnormal temperature threshold, a mitigation controller that is actuated by the power source, and a plurality of local temperature sensors that are communicatively coupled to the mitigation controller and are arranged for detecting critical temperatures in specific regions of the environment. The mitigation controller executes a mitigation action when one of the critical temperatures exceeds a predetermined critical temperature threshold for the corresponding specific region.