DocumentCode :
831495
Title :
Improving Radiation Tolerance in Space-Borne Electronics
Author :
Holmes-Siedle, Andrew ; Freeman, R.F.A.
Author_Institution :
Fulmer Research Institute Limited, Stoke Poges, Slough SL2 4QD, England
Volume :
24
Issue :
6
fYear :
1977
Firstpage :
2259
Lastpage :
2265
Abstract :
The Complementary Metal-Oxide-Semiconductor (CMOS) device is a very desirable form of technology for space use despite the low tolerance to radiation exhibited by current commercial samples. It is thus important to establish "hardness engineering" methods for systems employing these devices. It is necessary to deploy a wide variety of design methods to prolong the life of many present-day CMOS circuits. An original ranking scheme for various forms of CMOS technology is proposed, as are design rules for the layout of the spacecraft equipment platforms and of circuit elements within equipment boxes. Limitation of the electrical stress cycles applied to devices is shown to prolong life greatly. The addition of deadweight shielding is treated as a last resort. Design rules and formulae are emerging which enable the spacecraft designer to minimise added weight and maximise the life of the space vehicle.
Keywords :
Aerospace electronics; Aerospace engineering; Aluminum; CMOS technology; Circuits; Large scale integration; MOS devices; Satellites; Space technology; Space vehicles;
fLanguage :
English
Journal_Title :
Nuclear Science, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9499
Type :
jour
DOI :
10.1109/TNS.1977.4329203
Filename :
4329203
Link To Document :
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