"A Practical Approach to the Optimization of the Saturn V Space Vehicle Control System Under Aerodynamic Loads."
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.
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| Format: | Electronic |
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University of Alabama in Huntsville Archives
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| Online Access: | http://libarchstor2.uah.edu/digitalcollections/items/show/2337 |
