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NASA NTRS · 19650010305

Thermal conditions during typical boost trajectory

Roudebush, W. H.

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Abstract

Aerodynamic heating calculation of Atlas Centaur launch vehicle trajectory

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TRAJECTORY ATLAS CENTAUR LAUNCH VEHICLE AERODYNAMIC HEATING

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Roudebush, W. H.. 1965-03-01. Thermal conditions during typical boost trajectory. https://ntrs.nasa.gov/citations/19650010305

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