NASA NTRS · 19730013085
Structural load reduction of the space shuttle booster/orbiter configuration using a load relief guidance technique
Abstract
A space shuttle booster/orbiter atmospheric ascent guidance algorithm is developed that will reduce the aerodynamically induced structural loads as compared to an open loop guidance algorithm.
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Deaton, A. W., Kelley, P. B.. 1973-04-05. Structural load reduction of the space shuttle booster/orbiter configuration using a load relief guidance technique. https://ntrs.nasa.gov/citations/19730013085
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