NASA NTRS · 19700028514
Abort separation including aerodynamic, dynamic, propulsive, and trajectory influences
Abstract
Aerodynamic effects on safe abort separation for space shuttles
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Decker, J. P., Mc Ghee, R. J., Pierpont, P. K.. 1970-07-01. Abort separation including aerodynamic, dynamic, propulsive, and trajectory influences. https://ntrs.nasa.gov/citations/19700028514
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