Abstract: A gimbal transmission cable management system is disclosed. The system can include a first gimbal portion and a second gimbal portion rotatable relative to one another to provide rotation about a gimbal axis. The system can also include a cable retainer fixed relative to one of the first and second gimbal portions and defining a cable volume between the cable retainer and at least one of the first and second gimbal portions. In addition, the system can include a transmission cable coiled about the gimbal axis within the cable volume. Bi-directional relative rotation of the first and second gimbal portions can alternately coil and uncoil a portion of the transmission cable about the gimbal axis within the cable volume.

Abstract: A gimbal transmission cable management system is disclosed. The system can include a first gimbal portion and a second gimbal portion rotatable relative to one another to provide rotation about a gimbal axis. The system can also include a cable retainer fixed relative to one of the first and second gimbal portions and defining a cable volume between the cable retainer and at least one of the first and second gimbal portions. In addition, the system can include a transmission cable coiled about the gimbal axis within the cable volume. Bi-directional relative rotation of the first and second gimbal portions can alternately coil and uncoil a portion of the transmission cable about the gimbal axis within the cable volume.

Abstract: A gimbal transmission cable management system is disclosed. The system can include a first gimbal portion and a second gimbal portion rotatable relative to one another to provide rotation about a gimbal axis. The system can also include a cable retainer fixed relative to one of the first and second gimbal portions and defining a cable volume between the cable retainer and at least one of the first and second gimbal portions. In addition, the system can include a transmission cable coiled about the gimbal axis within the cable volume. Bi-directional relative rotation of the first and second gimbal portions can alternately coil and uncoil a portion of the transmission cable about the gimbal axis within the cable volume.

Abstract: A gimbal transmission cable management system is disclosed. The system can include a first gimbal portion and a second gimbal portion rotatable relative to one another to provide rotation about a gimbal axis. The system can also include a cable retainer fixed relative to one of the first and second gimbal portions and defining a cable volume between the cable retainer and at least one of the first and second gimbal portions. In addition, the system can include a transmission cable coiled about the gimbal axis within the cable volume. Bi-directional relative rotation of the first and second gimbal portions can alternately coil and uncoil a portion of the transmission cable about the gimbal axis within the cable volume.

Abstract: The system includes a rotary turret platform for aiming of a high power laser beam. The system further includes a turret payload device coupled to the rotary turret platform. The system further includes an off-axis telescope coupled to the turret payload, having an articulated secondary mirror for correcting optical aberrations, and configured to reflect the high power laser beam to a target through a first of at least two conformal windows. The system further includes an illuminator beam device configured to actively illuminating the target to generate a return aberrated wavefront through the first of the at least two conformal windows. The system further includes a coarse tracker coupled to the turret payload, positioned parallel to and on an axis of revolution of the off-axis telescope, and configured to detect, acquire, and track the target through the second of the at least two conformal windows.

Abstract: The technology can include a retractable rotary turret system. The system includes a base comprising two support arms. The system further includes a turret platform that is a truncated sphere having a substantially flat side and a substantially spherical side. The turret platform includes a turret support ring rotary coupled to the two support arms and a turret device isolatively coupled to the turret support ring. The turret platform is rotatable along a first dimension for deployment of the spherical side and is rotatable along the first dimension for deployment of the flat side.

Abstract: The technology can include a high power laser beam delivery system. The system includes a rotary turret platform rotatable along multiple axes for aiming of a high power laser beam. The system further includes a turret payload device coupled to the rotary turret platform that is a truncated sphere and configured to rapidly deploy from a vehicle and stow within the vehicle. The system further includes at least two conformal windows in a spherical side of the turret payload. The system further includes an off-axis telescope coupled to the turret payload, having an articulated secondary mirror for correcting optical aberrations, and configured to reflect the high power laser beam to a target through the first of the at least two conformal windows.

Abstract: The technology can include a retractable rotary turret system. The system includes a base comprising two support arms. The system further includes a turret platform that is a truncated sphere having a substantially flat side and a substantially spherical side. The turret platform includes a turret support ring rotary coupled to the two support arms and a turret device isolatively coupled to the turret support ring. The turret platform is rotatable along a first dimension for deployment of the spherical side and is rotatable along the first dimension for deployment of the flat side.

Abstract: An adjustable fixture for mounting any of a plurality of weapon sets to an aircraft includes a bracket and lugs that are adjustably mechanically coupled to the bracket. The fixture may be adjusted once, to achieve proper orientation relative to the aircraft for boresighting, and may thereafter allow switching of weapon sets, either of the same type or of different types, without a need for re-boresighting. Quick-release fasteners, such as quick-release pins, may be used to couple the weapon sets to the fixture, to allow for easy and rapid change of weapon stores. The fixture may include one or more adapters used to allow various kinds of weapon sets to be coupled to the bracket.

Abstract: An adjustable fixture for mounting any of a plurality of weapon sets to an aircraft includes a bracket and lugs that are adjustably mechanically coupled to the bracket. The fixture may be adjusted once, to achieve proper orientation relative to the aircraft for boresighting, and may thereafter allow switching of weapon sets, either of the same type or of different types, without a need for re-boresighting. Quick-release fasteners, such as quick-release pins, may be used to couple the weapon sets to the fixture, to allow for easy and rapid change of weapon stores. The fixture may include one or more adapters used to allow various kinds of weapon sets to be coupled to the bracket.