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Analysis of propellant slosh dynamics and generation of an equivalent mechanical model for use in preliminary voyager autopilot design studiesLinearized dynamic equations and mechanical model for propellant sloshing in Lunar Excursion Module Descent Propulsion System /LEMDPS/
Document ID
19680017770
Document Type
Contractor Report (CR)
Authors
Lance, T. A. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 4, 2013
Publication Date
December 1, 1966
Subject Category
PROPELLANTS
Report/Patent Number
JPL-TM-33-306
NASA-CR-95147
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Public Use Permitted.

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