NASA NTRS · 19680024284
Load relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements
Abstract
Load relief autopilot to minimize launch vehicle thrust vector deflection angle required for vehicle stability during flight through design winds
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Scalzott, L. L., Teren, F.. 1968-09-01. Load relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements. https://ntrs.nasa.gov/citations/19680024284
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