Abstract: A Fiber Bragg grating (FBG) sensor structure, a method of fabricating a FBG sensor structure, and a method of employing a FBG sensor structure comprising an optical fiber portion having at least one FBG formed therein. The FBG sensor structure comprises an optical fiber portion having at least one FBG formed therein; and a sleeve structure capable of transferring vibrations and/or strain along a length thereof; wherein the optical fiber portion is coupled to the sleeve structure such that the central wavelength of the FBG, is variable under the transferred vibrations and/or strain.

Abstract: A control moment gyroscope (CMG) module for use in a satellite comprising a CMG, the CMG comprising a flywheel assembly mounted on a gimbal assembly, the flywheel assembly comprising a flywheel rim, a flywheel spokes member and a flywheel shaft, the flywheel rim circumscribing the flywheel shaft, and the flywheel spokes member extending between the flywheel shaft and the flywheel rim. The gimbal assembly comprises at least one gimbal and a spin motor, the spin motor for rotating the flywheel assembly about a first axis. The CMG further comprises a torque shaft and a torque motor for rotating the at least one gimbal about a second axis. The CMG module further comprises a hermetic first shell housing; and a hermetic second shell housing; wherein the second shell housing is joined to the first shell housing by a hermetic seal to form an airtight interior of the CMG module, the interior of the CMG module containing the CMG.

Abstract: A control moment gyroscope (CMG) module for use in a satellite comprising a CMG, the CMG comprising a flywheel assembly mounted on a gimbal assembly, the flywheel assembly comprising a flywheel rim, a flywheel spokes member and a flywheel shaft, the flywheel rim circumscribing the flywheel shaft, and the flywheel spokes member extending between the flywheel shaft and the flywheel rim. The gimbal assembly comprises at least one gimbal and a spin motor, the spin motor for rotating the flywheel assembly about a first axis. The CMG further comprises a torque shaft and a torque motor for rotating the at least one gimbal about a second axis. The CMG module further comprises a hermetic first shell housing; and a hermetic second shell housing; wherein the second shell housing is joined to the first shell housing by a hermetic seal to form an airtight interior of the CMG module, the interior of the CMG module containing the CMG.

Abstract: A portable satellite antenna terminal, comprising a body and a unit within the body for controlling the terminal and terminal functions. Also provided is an antenna mounted to the body for movement relative thereto. The antenna is able to be stowed within the body when not in use. The antenna may be a flat panel antenna and is moveable relative to the body from a stowed position to an in-use position.

Abstract: A portable satellite antenna terminal, comprising a body (620) and a unit (637) within the body (620) for controlling the terminal and terminal functions. Also provided is an antenna (607) mounted to the body (620) for movement (633, 635) relative thereto. The antenna (607) is able to be stowed within the body (620) when not in use. The antenna (607) may be a flat panel antenna (624) and is moveable relative to the body (620) from a stowed position to an in-use position.

Abstract: A portable satellite antenna terminal, comprising a body (620) and a unit (637) within the body (620) for controlling the terminal and terminal functions. Also provided is an antenna (607) mounted to the body (620) for movement (633, 635) relative thereto. The antenna (607) is able to be stowed within the body (620) when not in use. The antenna (607) may be a flat panel antenna (624) and is moveable relative to the body (620) from a stowed position to an in-use position.