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NESC Technical Bulletin 22-03: Treatment of Transient Pressure Events in Space Flight Pressurized SystemsAnalytical and experimental evidence shows that fast-moving dynamic pressure fluctuations caused by valve actuation,
fluid system priming, fluid discharge, vibration, and flow disturbances can elicit adverse structural response and must
be considered in the space flight pressure system verification process.
Document ID
20220006583
Acquisition Source
Langley Research Center
Document Type
Other - NESC Technical Bulletin No. 22-03
Authors
Kauser Imtiaz (Johnson Space Center Houston, Texas, United States)
Date Acquired
April 28, 2022
Publication Date
May 12, 2022
Subject Category
Mechanical Engineering
Funding Number(s)
WBS: 869021.01.23.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Transient Pressure
Propulsion Systems
Pressurized Systems
NESC
Technical Bulletin No. 22-03

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