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ANSI/AIAA S-142-2016

Handbook for Multipactor Breakdown Prevention in Spacecraft Components

This document is intended to provide a standardized process for mitigation of multipactor breakdown within spacecraft components. It is directed toward component designers, satellite system engineers, as well as the customer community to provide worst-case conditions, margin requirements, and verification of those requirements using state-of-the-art methodologies. In addition, recommended methods are provided, with examples, to ensure proper requirement verification for all satellite RF components susceptible to RF breakdown

CONTENT PROVIDER
American Institute of Aeronautics and Astronautics [aiaa]

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