NASA NTRS · 19750012376
Aerodynamic and base heating studies on space shuttle configurations
Abstract
Heating rate and pressure measurements were obtained on a 25-O space shuttle model in a vacuum chamber. Correlation data on windward laminar and turbulent boundary layers and leeside surfaces of the space shuttle orbiter are included.
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1974-11-01. Aerodynamic and base heating studies on space shuttle configurations. https://ntrs.nasa.gov/citations/19750012376
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