Abstract: A calibration disc for providing uniform irradiance to an optical sensor system includes a first major surface, a second major surface opposite the first major surface, and an edge surface extending around a circumference of the calibration disc. The first major surface is fully reflective and partially diffuse, the second major surface is partially reflective and partially diffuse, and the edge surface is fully reflective and partially diffuse and has an entrance aperture positioned at the edge surface and configured to receive light into the calibration disc. The first major surface, the second major surface and the edge surface are configured to scatter the light received by the entrance aperture within the calibration disc. The second major surface is configured to emit at least some of the light with uniform irradiance.

Abstract: A calibration disc for providing uniform irradiance to an optical sensor system includes a first major surface, a second major surface opposite the first major surface, and an edge surface extending around a circumference of the calibration disc. The first major surface is fully reflective and partially diffuse, the second major surface is partially reflective and partially diffuse, and the edge surface is fully reflective and partially diffuse and has an entrance aperture positioned at the edge surface and configured to receive light into the calibration disc. The first major surface, the second major surface and the edge surface are configured to scatter the light received by the entrance aperture within the calibration disc. The second major surface is configured to emit at least some of the light with uniform irradiance.

Abstract: An apparatus includes multiple thermal interface segments collectively forming a discontinuous thermal interface configured to contact a curved surface of an object. The discontinuous thermal interface is configured to transfer thermal energy to or receive thermal energy from the curved surface of the object. Each of the thermal interface segments includes a major surface that is curved. The curved major surface of each of the thermal interface segments is configured to register with the curved surface of the object and has a specified area that is based on a Hertzian contact area defined partially by the curved surface of the object. The apparatus can also include a thermal gap pad configured to be compressed between the thermal interface segments and the object.

Abstract: The flexure mount system is disclosed that can accommodate thermal expansion. The flexure mount can include a base, a first flexure mount coupled to the base, a second flexure mount coupled to the base, and a supported structure coupled to the first and second flexure mounts along an axis. The first flexure mount can have a first radial flexure. The second flexure mount can have a second radial flexure and an axial flexure. The first and second radial flexures can be operable to provide radial compliance relative to the axis and the axial flexure can be operable to provide axial compliance parallel to the axis, such that the first flexure mount is radially compliant, and the second flexure mount is radially and axially compliant.

Abstract: The flexure mount system is disclosed that can accommodate thermal expansion. The flexure mount can include a base, a first flexure mount coupled to the base, a second flexure mount coupled to the base, and a supported structure coupled to the first and second flexure mounts along an axis. The first flexure mount can have a first radial flexure. The second flexure mount can have a second radial flexure and an axial flexure. The first and second radial flexures can be operable to provide radial compliance relative to the axis and the axial flexure can be operable to provide axial compliance parallel to the axis, such that the first flexure mount is radially compliant, and the second flexure mount is radially and axially compliant.

Abstract: An apparatus includes multiple thermal interface segments collectively forming a discontinuous thermal interface configured to contact a curved surface of an object. The discontinuous thermal interface is configured to transfer thermal energy to or receive thermal energy from the curved surface of the object. Each of the thermal interface segments includes a major surface that is curved. The curved major surface of each of the thermal interface segments is configured to register with the curved surface of the object and has a specified area that is based on a Hertzian contact area defined partially by the curved surface of the object. The apparatus can also include a thermal gap pad configured to be compressed between the thermal interface segments and the object.

Abstract: A system includes a pulse tube, a compressor configured to create pulses of fluid in the pulse tube, and a surge tank. The surge tank includes a housing that defines a surge volume configured to receive the fluid from the pulse tube. An inertance channel defines a passageway through which the fluid flows to and from the surge volume. At least part of the inertance channel has an open side to the surge volume. The surge tank also includes an adjustable seal configured to block at least part of the open side of the inertance channel and to move in order to change a functional length of the inertance channel. The housing may include a material having a high coefficient of thermal expansion, and the adjustable seal may include a material having a low coefficient of thermal expansion.

Abstract: A system includes a pulse tube, a compressor configured to create pulses of fluid in the pulse tube, and a surge tank. The surge tank includes a housing that defines a surge volume configured to receive the fluid from the pulse tube. An inertance channel defines a passageway through which the fluid flows to and from the surge volume. At least part of the inertance channel has an open side to the surge volume. The surge tank also includes an adjustable seal configured to block at least part of the open side of the inertance channel and to move in order to change a functional length of the inertance channel. The housing may include a material having a high coefficient of thermal expansion, and the adjustable seal may include a material having a low coefficient of thermal expansion.

Abstract: In one or more embodiments, a multi-axis articulated solar light shade that protects elements of a space-based sensor from direct solar illumination includes a base; a partial conical baffle tube having a first end portion, a second end portion, an elongated curved portion defining a shade between the first and second end portions, and an opening defined in an interior of the elongated curved portion, the first end portion rotatably attached to the base; and a visor pivotably attached to the second end portion. The partial conical baffle tube may be selectively rotated about a sensor line-of-sight in response to the sun's position relative to the sensor line-of-sight; and the visor may be selectively pivoted relative to the partial conical baffle tube in response to the sun's position relative to the sensor line-of-sight so as to protect the sensor from the direct solar illumination at any given time or any given orbital position.

Abstract: In one or more embodiments, a multi-axis articulated solar light shade that protects elements of a space-based sensor from direct solar illumination includes a base; a partial conical baffle tube having a first end portion, a second end portion, an elongated curved portion defining a shade between the first and second end portions, and an opening defined in an interior of the elongated curved portion, the first end portion rotatably attached to the base; and a visor pivotably attached to the second end portion. The partial conical baffle tube may be selectively rotated about a sensor line-of-sight in response to the sun's position relative to the sensor line-of-sight; and the visor may be selectively pivoted relative to the partial conical baffle tube in response to the sun's position relative to the sensor line-of-sight so as to protect the sensor from the direct solar illumination at any given time or any given orbital position.