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Dynamic stability of space vehicles. Volume 14 - Testing for booster propellant sloshing parametersRecommended procedures for stability, control, and structural loading analysis of large liquid fueled rocket booster sloshing parameters
Document ID
19680013985
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Eggleston, D. M. (General Dynamics Corp. San Diego, CA, United States)
Date Acquired
August 4, 2013
Publication Date
May 1, 1968
Publication Information
Publisher: NASA
Subject Category
Structural Mechanics
Report/Patent Number
GD/C-BTD-67-089, V. 14
NASA-CR-948
Report Number: GD/C-BTD-67-089, V. 14
Report Number: NASA-CR-948
Accession Number
68N23454
Funding Number(s)
CONTRACT_GRANT: NAS8-11486
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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