Abstract: A method making a gun barrel liner includes depositing material on a mandrel that has ribs or ridges corresponding to the rifling grooves in the liner. The material may be deposited using plasma spraying, with sprayed splats of material re-melted after deposition for at least part of the deposition process to reduce or eliminate porosity in the deposited material. The mandrel may be made of metal, such as a high thermal conductivity metal such as copper. The mandrel may have a channel therein or therethrough. The channel may facilitate flow of liquid though the mandrel, one example of such a liquid being a coolant (such as water), used to remove heat produced during the material deposition. Another liquid passed through the channel may be an etchant (or other fluid) that is used to dissolve or otherwise remove the mandrel after the material of the gun barrel liner has been deposited.

Abstract: A method of forming of an item includes: selecting a component of the item that is formed of an element; mixing one or more identifiable additives with the element; forming the component with the mixture; performing an atomic level test on at least a portion of the component; and recording the results of the test.

Abstract: A method of forming of an item includes: selecting a component of the item that is formed of an element; mixing one or more identifiable additives with the element; forming the component with the mixture; performing an atomic level test on at least a portion of the component; and recording the results of the test.

Abstract: A scanning telescope including an on-axis four-mirror reflective telescope configured to receive electromagnetic radiation through an optical aperture and to direct and focus the electromagnetic radiation onto an imaging detector, the on-axis four-mirror reflective telescope including a rear-most mirror configured to be movable over a range of angular tilt relative to an optical axis of the scanning telescope to scan a field of view of the imaging detector over a scan range. In one example, the rear-most scanning mirror is the tertiary mirror of the four-mirror reflective telescope, and all four mirrors are axisymmetric about the optical axis of the telescope.

Abstract: A scanning telescope including an on-axis four-mirror reflective telescope configured to receive electromagnetic radiation through an optical aperture and to direct and focus the electromagnetic radiation onto an imaging detector, the on-axis four-mirror reflective telescope including a rear-most mirror configured to be movable over a range of angular tilt relative to an optical axis of the scanning telescope to scan a field of view of the imaging detector over a scan range. In one example, the rear-most scanning mirror is the tertiary mirror of the four-mirror reflective telescope, and all four mirrors are axisymmetric about the optical axis of the telescope.

Abstract: A system and method for joining together a pair of brittle material pieces, such as controlled expansion ceramic pieces, involves using a threaded plug joined to a first brittle material piece, to secure a threaded fastener passing through part of the second brittle material piece, thus joining together the brittle material pieces. The threaded plug may be inserted in a plug-receiving hole that may be substantially perpendicular to a fastener-receiving hole in the first brittle material piece. One or both of the plug and the plug-receiving hole may be conical, to facilitate fitting the plug into the plug-receiving hole. The plug may be secured to the first brittle piece by soldering. The system and method provides a secure way of threadedly joining together a pair of brittle material parts, without use of possibly contaminating adhesives, and without a need to put threads on the actual brittle material itself.

Abstract: The 6-axis position and attitude of an imaging vehicle's detector assembly is measured by mounting the detector assembly on a compliant isolator and separating the main 6-axis IMU on the vehicle from a secondary IMU comprising at least inertial rate sensors for pitch and yaw on the detector assembly. The compliant isolator couples low-frequency rigid body motion of the vehicle below a resonant frequency to the isolated detector assembly while isolating the detector assembly from high-frequency attitude noise above the resonant frequency. A computer processes measurements of the 6-axis rigid body motion and the angular rate of change in yaw and pitch of the isolated detector assembly to mitigate the drift and noise error effects of the secondary inertial rate sensors and estimate the 6-axis position and attitude of the detector assembly.

Abstract: The 6-axis position and attitude of an imaging vehicle's detector assembly is measured by mounting the detector assembly on a compliant isolator and separating the main 6-axis IMU on the vehicle from a secondary IMU comprising at least inertial rate sensors for pitch and yaw on the detector assembly. The compliant isolator couples low-frequency rigid body motion of the vehicle below a resonant frequency to the isolated detector assembly while isolating the detector assembly from high-frequency attitude noise above the resonant frequency. A computer processes measurements of the 6-axis rigid body motion and the angular rate of change in yaw and pitch of the isolated detector assembly to mitigate the drift and noise error effects of the secondary inertial rate sensors and estimate the 6-axis position and attitude of the detector assembly.

Abstract: The 6-axis position and attitude of an imaging vehicle's detector assembly is measured by mounting the detector assembly on a compliant isolator and separating the main 6-axis IMU on the vehicle from secondary inertial rate sensors on the detector assembly. The compliant isolator couples low-frequency rigid body motion of the vehicle below a resonant frequency to the isolated detector assembly while isolating the detector assembly from high-frequency attitude noise above the resonant frequency. The secondary inertial rate sensors measure the angular rate of change in yaw and pitch of the isolated detector assembly. A computer processes measurements of the 6-axis rigid body motion and the angular rate of change in yaw and pitch of the isolated detector assembly to estimate the 6-axis position and attitude of the detector assembly.

Abstract: The 6-axis position and attitude of an imaging vehicle's detector assembly is measured by mounting the detector assembly on a compliant isolator and separating the main 6-axis IMU on the vehicle from secondary inertial rate sensors on the detector assembly. The compliant isolator couples low-frequency rigid body motion of the vehicle below a resonant frequency to the isolated detector assembly while isolating the detector assembly from high-frequency attitude noise above the resonant frequency. The secondary inertial rate sensors measure the angular rate of change in yaw and pitch of the isolated detector assembly. A computer processes measurements of the 6-axis rigid body motion and the angular rate of change in yaw and pitch of the isolated detector assembly to estimate the 6-axis position and attitude of the detector assembly.

Abstract: A kinetic anti-projectile vehicle includes a body, and extendible arms that extend radially from the body. The arms include a foam material, such as a shape memory foam. The foam material may be heated to expand it. The foam arms may be mechanically restrained while being heated. The mechanically restraint may be removed by heating, for example including a fusible link or a shape memory sold material. The foam material arms may include solid material, either in the form of solid material particles, such as high strength particles, or in the form of supports or restraints in the foam material. The extension of the foam arms increases the effective area of the vehicle for impacting a projectile. Impact on the projectile from the body and/or one or more of the arms may be sufficient to destroy, divert, or otherwise disable the projectile.

Abstract: A kinetic anti-projectile vehicle includes a body, and extendible arms that extend radially from the body. The arms include a foam material, such as a shape memory foam. The foam material may be heated to expand it. The foam arms may be mechanically restrained while being heated. The mechanically restraint may be removed by heating, for example including a fusible link or a shape memory sold material. The foam material arms may include solid material, either in the form of solid material particles, such as high strength particles, or in the form of supports or restraints in the foam material. The extension of the foam arms increases the effective area of the vehicle for impacting a projectile. Impact on the projectile from the body and/or one or more of the arms may be sufficient to destroy, divert, or otherwise disable the projectile.

Abstract: A method of adjusting an optical system includes placing the optical system in a controlled environment enclosure, and adjusting an optical mount of the optical system while the optical system is in the controlled environment enclosure.

Abstract: A system and method for joining together a pair of brittle material pieces, such as controlled expansion ceramic pieces, involves using a threaded plug joined to a first brittle material piece, to secure a threaded fastener passing through part of the second brittle material piece, thus joining together the brittle material pieces. The threaded plug may be inserted in a plug-receiving hole that may be substantially perpendicular to a fastener-receiving hole in the first brittle material piece. One or both of the plug and the plug-receiving hole may be conical, to facilitate fitting the plug into the plug-receiving hole. The plug may be secured to the first brittle piece by soldering. The system and method provides a secure way of threadedly joining together a pair of brittle material parts, without use of possibly contaminating adhesives, and without a need to put threads on the actual brittle material itself.