Actions for Computer program provides improved longitudinal response analysis for axisymmetric launch vehicles

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Computer program provides improved longitudinal response analysis for axisymmetric launch vehicles

Author
Smith, W. W.
Published
Dec 1, 1967.
Physical Description
1 electronic document
Additional Creators
Walton, W. C., Jr.
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Computer program calculates axisymmetric launch vehicle steady-state response to axisymmetric sinusoidal loads. A finite element technique is utilized to construct the total launch vehicle stiffness matrix and mass matrix by subdividing the prototype structure into a set of axisymmetric shell components, fluid components, and spring-mass components.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19670000530.
Accession ID: 67B10531.
LAR-10093.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 16210239