Electromagnetic emission experiences using electric propulsion systems - A surveyAs electric propulsion systems become ready to integrate with spacecraft systems, the impact of propulsion system radiated emissions are of significant interest. Radiated emissions from electromagnetic, electrostatic, and electrothermal systems have been characterized and results synopsized from the literature describing 21 space flight programs. Electromagnetic radiated emission results from ground tests and flight experiences are presented with particular attention paid to the performance of spacecraft subsystems and payloads during thruster operations. The impacts to transmission of radio frequency signals through plasma plumes are also reviewed.
Document ID
19870062921
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sovey, James S. (NASA Lewis Research Center Cleveland, OH, United States)
Zana, Lynnette M. (NASA Lewis Research Center Cleveland, OH, United States)
Knowles, Steven C. (Rocket Research Co. Redmond, WA, United States)