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NASA Engineering and Safety Center Technical Bulletin No. 22-06: Treatment of Slosh Stability Margin Reductions for Human-Rated Launch VehiclesSlosh dynamics pose a stability concern for human-rated launch vehicles during ascent. Historical perspectives on the treatment of slosh dynamics, newly developed rules of thumb, the utility of flight data, and methods for analyzing and dispositioning slosh instability risks should be considered when linear stability margins are lower than typically accepted for human-rated systems.
Document ID
20220011709
Acquisition Source
Langley Research Center
Document Type
Other - NESC Technical Bulletin
Authors
Tannen S. VanZwieten
(Kennedy Space Center Merritt Island, Florida, United States)
Cornelius J. Dennehy
(Goddard Space Flight Center Greenbelt, Maryland, United States)
John H. Wall
(Jacobs (United States) Dallas, Texas, United States)
Date Acquired
August 2, 2022
Publication Date
August 8, 2022
Subject Category
Launch Vehicles And Launch Operations
Funding Number(s)
WBS: 869021.01.23.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Fuel Slosh
Slosh Stability
GN&C Gain and Phase Margins
Human-Rated Launch Vehicles
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