Marshall Technical Reports Server

Specification, Measurement, and Control of Electrical Switching Transients

NASA/CR-1999-209574, Javor, K., Specification, Measurement, and Control of Electrical Switching Transients, NASA's Space Environments and Effects (SEE) Program, Technical Monitor: Dawn Trout, NASA Marshall Space Flight Center, Alabama 35812, and EMC Compliance, P.O. Box 14161, Huntsville, AL 35815-0161, September, 1999, pp. 51, Format(s): PDF 5136k

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There have been several instances of susceptibility to switching transients. The Space Shuttle Spacelab Remote Acquisition Unit (RAU-a standard interface between Spacelab payloads and the Shuttle communication system) will shut down if the input 28 Vdc bus drops below 22 volts for more than 80 gs. Although a MIL-STD-461 derivative CS06 requirement was levied on the RAU, it failed to find this susceptibility. A heavy payload on one aircraft sags the 28 volt bus below 20 volts for milliseconds. Dc-dc converters have an operating voltage. A typical 28 Vdc-to-5 Vdc converter operates within tolerance when input potential is between 17-40 Vdc. A hold-up capacitor can be used to extend the time this range is presented to the converter when the line potential sags or surges outside this range. The designer must know the range of normal transients in order to choose the correct value of hold-up. This report describes the phenomena of electrical power bus transients induced by the switching of loads both on and off the bus, and control thereof.
Keywords:switching transients, transient switching control, power bus transients
Subjects:Engineering: Electronics and Electrical Engineering: Electronic Components
ID Code:466
Deposited On:12 July 2002