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- W202205514 abstract "This paper discusses some of the special factors encountered in the design of digital systems for space environment. Unique challenges are presented to the design engineer due to the requirements of ultra-reliability, minimum power, weight, and volume, and environmental considerations including shock, vibration, temperature, and prolonged exposure to radiation and vacuum. These requirements present changes both of degree and of fundamental concept from those of the standard ground based system. The circuitry used in the Scientific Data Conditioning System on board the Mariner II spacecraft is described to illustrate one approach to the design of low power, high reliability equipment. The system controlled the sampling of all Mariner scientific experiments, prepared the data for transmission, and generated special instrumentation control and calibration signals. Several other circuits are discussed to indicate other sets of compromises made in the design of both space-borne and ground based systems. Some conclusions are drawn then to indicate possible trends in the design of spacecraft data handling equipment, and the potential role of microelectronics in this area." @default.
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- W202205514 date "1964-01-01" @default.
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- W202205514 title "DESIGNING MINIMUM POWER DIGITAL CIRCUITS FOR MARINER II AND OTHER SPACECRAFTS" @default.
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- W202205514 doi "https://doi.org/10.1016/b978-0-08-010625-0.50011-2" @default.
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