Load relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements
1968
II, 39 S
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
DSpace@MIT | 1976
|VERSATILE LAUNCH VEHICLE DIGITAL AUTOPILOT*
SAE Technical Papers | 1969
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