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Equations for two-dimensional analysis of touchdown dynamics of spacecraft with hinged legs including elastic, damping, and crushing effectsEquations for two-dimensional analysis of elastic, damping, and crushing effects from spacecraft lunar landing
Document ID
19660014379
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lavender, R. E. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
November 6, 1963
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-57404
MTP-AERO-63-76
Accession Number
66N23668
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LUNAR LANDING
SPACECRAFT LANDING
MOTION EQUATION

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