Airvolt Aircraft Electric Propulsion Test Stand

Samuel, Aamod; Lin, Yohan

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NASA NTRS · 20160001339

Airvolt Aircraft Electric Propulsion Test Stand

Samuel, Aamod·Lin, Yohan

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Abstract

Development of an electric propulsion test stand that collects high-fidelity data of motor, inverter, and battery system efficiencies; thermal dynamics; and acoustics independent of manufacturer reported values will improve understanding of electric propulsion systems to be used in future aircraft. A buildup approach to this development reveals new areas of research and best practices in testing, and attempts to establish a standard for testing these systems.

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Samuel, Aamod, Lin, Yohan. 2015-07-27. Airvolt Aircraft Electric Propulsion Test Stand. https://ntrs.nasa.gov/citations/20160001339

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