Nobles R A, Acton L W, Joki E G, Leibacher J W, Peterson R C
Appl Opt. 1980 Sep 1;19(17):2957-66. doi: 10.1364/AO.19.002957.
A description is presented of a flight-qualified large-aperture 12 x 12-sec of arc angular resolution multigrid x-ray collimator developed for the Solar Maximum Mission (SMM) flat crystal spectrometer. This collimator, designed for the 1.4-22.4-A wavelength range, utilizes an optical bench/metering structure to align and support prealigned grid subassemblies. One advantage of this scheme is to provide ready access to the grid subassemblies for inspection and/or servicing. The optical bench is a lightweight, rigid, and stable aluminum honeycomb structure. Aluminum is a viable material choice in this application because of the good thermal control expected in the SMM instrument package. The grids are of a compound and bimetallic design, having 63.5-microm square holes on an 88.9-microm spacing in 8-microm thick gold, which is in turn supported by a 76-microm thick Invar grid having 600-microm square holes on a 739-microm spacing. The small apertures in the gold provide the 12-sec of arc collimation with the Invar grids providing wide angle off-axis blocking out to an ~35-min of arc view angle. The collimator has seven individual channels, four of a 5.1- x 10-cm area and three of a 1.3- x 10-cm area. Laboratory measurements gave an average angular resolution of 12.5-sec of arc FWHM with 0.259 transmission for the large area channels and 12.0 sec of arc and 0.200 transmission for the small area channels. A hypothetical perfectly aligned collimator would have 12.5-sec of arc resolution and 0.300 transmission. A thermal filter composed of two layers of ~1000-A thick aluminum prevents solar heating of the front collimator grids by absorbing longer wavelength radiation while passing most of the x radiation in the band of interest. The filter was flight qualified by passing a protoflight acoustic test environment of 147-dB total sound level, 20-microN/M(2) reference, for 1-min duration.
本文介绍了一种为太阳峰年使命(SMM)平晶光谱仪研制的、具备飞行资格的大孔径12×12弧秒角分辨率多栅格X射线准直器。该准直器专为1.4 - 22.4埃波长范围设计,利用光学平台/测量结构来对准并支撑预先对准的栅格子组件。此方案的一个优点是便于对栅格子组件进行检查和/或维修。光学平台是一种轻质、刚性且稳定的铝蜂窝结构。在该应用中,铝是一种可行的材料选择,因为SMM仪器包预期具有良好的热控制。这些栅格采用复合和双金属设计,在8微米厚的金层上有间距为88.9微米的63.5微米见方的孔,该金层又由76微米厚的因瓦合金栅格支撑,因瓦合金栅格上有间距为739微米的600微米见方的孔。金层中的小孔提供12弧秒的准直,因瓦合金栅格提供广角离轴阻挡,视场角可达约35弧分。该准直器有七个独立通道,四个通道面积为5.1×10平方厘米,三个通道面积为1.3×10平方厘米。实验室测量结果显示,大面积通道的半高宽平均角分辨率为12.5弧秒,透过率为0.259;小面积通道的角分辨率为12.0弧秒,透过率为0.200。一个假设的完美对准的准直器将具有12.5弧秒的分辨率和0.300的透过率。一个由两层约1000埃厚的铝组成的热滤光片,通过吸收较长波长的辐射,同时使感兴趣波段的大部分X射线通过,防止前准直器栅格受到太阳加热。该滤光片通过了原飞行声学测试环境,总声级为147分贝,参考值为20微牛/平方米,持续时间为1分钟,从而具备飞行资格。