Crystal module and satellite-borne space photoelectric detection unit comprising crystal module
A photoelectric detection and crystal technology, applied in the field of space detection, can solve problems such as high quality, achieve the effects of improving inheritance, shortening the development cycle, and ensuring usability
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Embodiment 1
[0060] like Figure 1 to Figure 5 A crystal module shown in a space-borne photoelectric detection unit includes crystal 109, a crystal protection structure, a temperature detection structure, a performance calibration structure, and an installation interface.
[0061] The crystal protection structure includes a shell 101, an end cap 103 and a quartz glass sheet 106. In this embodiment, the shell 101 and the end cap 103 are made of aluminum. In order to further reduce the structural quality, a magnesium alloy may be considered.
[0062] The tube shell 101 has a T-shaped shape, the upper part is a head, which is connected with the photoelectric conversion module, and is in the shape of a rectangular block, and the lower part is a cylindrical tube body, and the head and the tube body are integrally formed. The shell 101 is provided with a cylindrical body cavity, and the crystal 103 is installed in the body cavity.
[0063] The end cap 103 is composed of an integrally formed cov...
Embodiment 2
[0077] like Figure 14 to Figure 17 A space-borne photoelectric detection unit shown includes a crystal module 1 and a photoelectric conversion module 2 . The structural design of the crystal module 1 is the same as that in Embodiment 1, and the structure of the photoelectric conversion module 2 is as follows Figure 7 to Figure 13 As shown, it includes a photoelectric conversion device 205, an electronic readout circuit board 201 (hereinafter referred to as a PCB board) and a protective structure.
[0078] The photoelectric conversion device 205 is used to convert the flash light emitted by the crystal 109 into photoelectrons. In this embodiment, a more commonly used photomultiplier tube (PMT) is used. Since it is a glass device, the space-borne device needs to experience extremely strong mechanical forces. Vibration environment, so buffer glue 204 is needed to protect it.
[0079] The protective structure also includes an inner bushing 207, a magnetic shielding device 206,...
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