CCDs and camera electronics for the NASA CONTOUR mission

被引：3

作者：

Darlington, EH ^{[1
]}

Grey, MP ^{[1
]}

机构：

[1] Johns Hopkins Univ, Appl Phys Lab, Laurel, MD 20723 USA

来源：

UV/EUV AND VISIBLE SPACE INSTRUMENTATION FOR ASTRONOMY AND SOLAR PHYSICS | 2001年 / 4498卷

关键词：

space; electronics; CCD; comet;

D O I：

10.1117/12.450056

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper addresses the imager designs for an upcoming NASA mission to examine comets at distances from the sun fairly similar to that of the earth. The general constraints oil design typical to a small spacecraft such as low mass and operation in vacuum apply. In addition the transient nature of the data which are presented as the spacecraft moves by the comet at high speed must be considered. Two imagers with different tasks to perform will be flown on this mission. Design choices for electronics and selection of charge coupled device image sensors are discussed. Some early results from breadboard tests are presented.

引用

页码：197 / 206

页数：10

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