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
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lance, T. A. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)