The application of integrated circuitry to spacecraft electronic systems is analyzed. The performance and characteristics of state-of-the art integrated circuits, including reliability and radiation resistance, have been determined. Both analog and digital integrated circuitry is evaluated. A comparison of integrated techniques (monolithic, thin-film, and hybrid) is made for the various requirements of spacecraft systems. (Author)
The Application of Integrated Circuitry to Spacecraft Electronic Systems
1965
34 pages
Report
No indication
English
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