Skip to content

Atlas / Learn / Papers / 20060037379

NASA NTRS · Preprint (Draft being sent to journal)

[No Title]

Published 2018-06-07 From Jet Propulsion Laboratory 1 author

Attribution

This is the abstract and citation. Full text lives at NASA NTRS — we link out rather than host. All credit to the authors and Jet Propulsion Laboratory.

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

Adequate performance was achieved relatively early in the development of ion engines and most subsequent development programs have focussed on demonstrating adequate engine life. The primary threats to engine reliability over the required service life are damage accumulation failure modes such as accelerator grid failure due to sputter erosion from charge exchange ions, erosion of discharge chamber components by lower energy ion sputtering and grid shorting by flakes of sputter-deposited material. These types of failure may typically be observed only after thousands of hours of operation. The purpose of this paper is to provide a critical review of the approaches used in past ion engine development programs to characterize and control these wearout failure mechanisms.

Author

  • Programs, The Role of Analysis;Testing Ion Engine Development

Keywords

  • Ion Engine

Citation: Programs, The Role of Analysis;Testing Ion Engine Development (2018). [No Title]. Jet Propulsion Laboratory. NASA NTRS ID 20060037379. https://ntrs.nasa.gov/citations/20060037379 ↗