"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.
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Electronic |
| Published: |
University of Alabama in Huntsville Archives
|
| Subjects: | |
| Online Access: | http://libarchstor2.uah.edu/digitalcollections/items/show/2337 |