DocumentCode :
912970
Title :
Total-Dose Failure Mechanisms of Integrated Circuits in Laboratory and Space Environments
Author :
Winokur, P.S. ; Sexton, F.W. ; Hash, G.L. ; Turpin, D.C.
Author_Institution :
Sandia National Laboratories Albuquerque, NM 87185
Volume :
34
Issue :
6
fYear :
1987
Firstpage :
1448
Lastpage :
1454
Abstract :
Total-dose failure mechanisms are identified over a wide range of dose rate for 2K and 16K SRAMs from hardened and commercial CMOS technologies. Failure was defined "parametrically," such that an IC fails if one of its parameters, e.g., static power supply current or timing, exceeds a preset specification following irradiation. These studies demonstrate that the dominant failure mechanisms of SRAMs in space radiation environments are often quite different than those observed at considerably higher laboratory dose rates specified by DoD test guidelines, i.e., 100 to 300 rad(Si)/s. In addition, the total-dose hardness of SRAMs varied significantly between laboratory and space dose rates. Several approaches are discussed for predicting total-dose hardness of ICs in space from laboratory measurements. Results are also presented for transistors irradiated over the same range of dose rate (200 to 0.02 rad(Si)/s) and at all biases, i.e., N-on/off and P-on/off. These transistor measurements are used to characterize the physical mechanisms that govern the radiation response of the more complex SRAMs. In a surprising result, a dose-rate dependence for the buildup of radiation-induced interface states was observed. At dose rates from 200 to 0.02 rad(Si)/s, the number of interface states at a given total dose increased as the dose rate decreased.
Keywords :
CMOS technology; Current supplies; Failure analysis; Integrated circuit technology; Interface states; Laboratories; Power supplies; Radiation hardening; Space technology; Timing;
fLanguage :
English
Journal_Title :
Nuclear Science, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9499
Type :
jour
DOI :
10.1109/TNS.1987.4337496
Filename :
4337496
Link To Document :
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