NASA NTRS · 19680054141
Simulation of the Apollo Command Module aerodynamics at re-entry altitudes.
Abstract
Apollo Command Module aerodynamics at reentry altitudes simulated by models in hypersonic flow
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Boylan, D. E., Griffith, B. J.. 1968-01-01. Simulation of the Apollo Command Module aerodynamics at re-entry altitudes.. https://ntrs.nasa.gov/citations/19680054141
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