DocumentCode
1947222
Title
Inverter matrix for the Clementine mission
Author
Buehler, M.G. ; Blaes, B.R. ; Tardio, G. ; Soli, G.A.
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear
1994
fDate
22-25 Mar 1994
Firstpage
198
Lastpage
203
Abstract
An inverter matrix test circuit was designed for the Clementine space mission and is built into the RRELAX (Radiation and Reliability Assurance Experiment). The objective is to develop a circuit that will allow the evaluation of the CMOS FETs using a lean data set in the noisy spacecraft environment. As is shown, only nine data points are needed to acquire ten CMOS FET parameters
Keywords
CMOS integrated circuits; insulated gate field effect transistors; integrated circuit testing; integrated logic circuits; logic arrays; logic testing; radiation effects; semiconductor device testing; CMOS FET parameters; Clementine space mission; RRELAX; Radiation and Reliability Assurance Experiment; inverter matrix test circuit; noisy spacecraft environment; Circuit testing; Extraterrestrial measurements; FETs; Geometry; Inverters; Laboratories; Propulsion; Space missions; Space vehicles; Threshold voltage;
fLanguage
English
Publisher
ieee
Conference_Titel
Microelectronic Test Structures, 1994. ICMTS 1994. Proceedings of the 1994 International Conference on
Conference_Location
San Diego, CA
Print_ISBN
0-7803-1757-2
Type
conf
DOI
10.1109/ICMTS.1994.303476
Filename
303476
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