spc_stnv_000109

"A Practical Approach to the Optimization of the Saturn V Space Vehicle Control System Under Aerodynamic Loads."

NASA TM X-53698

This paper includes the equations for the bending moment of a launch vehicle with the effects of bending and sloshing dynamics. It also includes a comparison between the bending moment response envelope of the measure winds and the bending moment response of the MSFC synthetic wind profile.

1965-07-21

Saturn V Collection

Box 14, Folder 30

University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama

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spc_stnv_000075_000118