Abstract: A laser weapon system is described. Particularly, embodiments describe subsystems of a laser weapon system including those necessary for laser generation, operational control, optical emission, and heat dissipation configured to provide a lightweight unit of reduced dimensions.

Abstract: A laser weapon system is described. Particularly, embodiments describe subsystems of a laser weapon system including those necessary for laser generation, operational control, optical emission, and heat dissipation configured to provide a lightweight unit of reduced dimensions.

Abstract: A laser weapon system is described. Particularly, embodiments describe subsystems of a laser weapon system including those necessary for laser generation, operational control, optical emission, and heat dissipation configured to provide a lightweight unit of reduced dimensions.

Abstract: A laser weapon system is described. Particularly, embodiments describe subsystems of a laser weapon system including those necessary for laser generation, operational control, optical emission, and heat dissipation configured to provide a lightweight unit of reduced dimensions.

Abstract: A laser weapon system is described. Particularly, embodiments describe subsystems of a laser weapon system including those necessary for laser generation, operational control, optical emission, and heat dissipation configured to provide a lightweight unit of reduced dimensions.

Abstract: A laser weapon system is described. Particularly, embodiments describe subsystems of a laser weapon system including those necessary for laser generation, operational control, optical emission, and heat dissipation configured to provide a lightweight unit of reduced dimensions.

Abstract: A laser weapon system is described. Particularly, embodiments describe subsystems of a laser weapon system including those necessary for laser generation, operational control, optical emission, and heat dissipation configured to provide a lightweight unit of reduced dimensions.

Abstract: An optical telescope is provided that includes a steering mirror configured to receive and redirect optical signals. The steering mirror is configured to be controllably oriented so as to control a direction in which the optical signals are redirected and to correspondingly control a line of sight. The optical telescope also includes a beam tube that includes a turning mirror configured to receive the optical signals from the steering mirror. The optical telescope also includes a primary mirror downstream of the turning mirror and configured to collimate the optical signals. Further, the optical telescope includes an output mirror configured to receive the optical signals from the primary mirror and to redirect the optical signals from the optical telescope. The output mirror is configured to be controllably oriented so as to control a direction in which the optical signals are redirected and to correspondingly control the line of sight.

Abstract: An optical telescope is provided that includes a steering mirror configured to receive and redirect optical signals. The steering mirror is configured to be controllably oriented so as to control a direction in which the optical signals are redirected and to correspondingly control a line of sight. The optical telescope also includes a beam tube that includes a turning mirror configured to receive the optical signals from the steering mirror. The optical telescope also includes a primary mirror downstream of the turning mirror and configured to collimate the optical signals. Further, the optical telescope includes an output mirror configured to receive the optical signals from the primary mirror and to redirect the optical signals from the optical telescope. The output mirror is configured to be controllably oriented so as to control a direction in which the optical signals are redirected and to correspondingly control the line of sight.

Abstract: A multifunction light detection and ranging (LIDAR) system for aircraft or other applications may use autodyne techniques. An autodyne system can use a single laser source and a single detector. The autodyne technique can mix two signal beams to produce a “beat note” at the frequency difference between the beams. Autodyne detection can leverage photon counting to support significantly reduced system complexity. Reduced complexity may provide solutions with significantly reduced power consumption, lighter weight, smaller volume, and lower cost. The multifunction LIDAR system can detect and identify regions of weather hazards such as lightning storms, aircraft wake vortex, clear air turbulence, and wind shear. The multifunction LIDAR system may also be configured to measure aircraft air and ground speed in multiple dimensions as well as aircraft altitude.

Abstract: A multifunction light detection and ranging (LIDAR) system for aircraft or other applications may use autodyne techniques. An autodyne system can use a single laser source and a single detector. The autodyne technique can mix two signal beams to produce a “beat note” at the frequency difference between the beams. Autodyne detection can leverage photon counting to support significantly reduced system complexity. Reduced complexity may provide solutions with significantly reduced power consumption, lighter weight, smaller volume, and lower cost. The multifunction LIDAR system can detect and identify regions of weather hazards such as lightning storms, aircraft wake vortex, clear air turbulence, and wind shear. The multifunction LIDAR system may also be configured to measure aircraft air and ground speed in multiple dimensions as well as aircraft altitude.