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Passivation of Spacecraft Pressure Vessels: Some Comments on Requirements, Principles, and PracticesMany space-faring organizations have requirements to limit the growth of orbital debris by passivating spacecraft that remain in orbit after mission end. These requirements state that a stored energy devices are to be fully depleted at the end of a spacecraft’s useful life. Spacecraft designs not able to comply with those requirements use a so-called “soft passivation” option. This report presents the results of two studies aimed at better understanding spacecraft pressure vessel passivation state-of-the-art. They summarize current practices and principles of pressure vessel passivation and present an approach that can be used to show that spacecraft propulsion system passivation has been achieved.
Document ID
20230014779
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
William Schonberg
(Missouri University of Science and Technology Rolla, Missouri, United States)
Scott Hull
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Date Acquired
October 12, 2023
Publication Date
October 1, 2023
Subject Category
Space Transportation and Safety
Report/Patent Number
NESC-TI-18-01367
Funding Number(s)
WBS: 869021.01.23.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Spacecraft Passivation
Micrometeoroid or Orbital Debris
Pressure Vessels
Fuel Tanks
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