NASA NTRS · 19690023917
Techniques developed to determine aerodynamic coefficients for Apollo applications program vehicles in an orbital environment
Abstract
Computer programs to determine aerodynamic coefficients for Apollo Applications Program vehicles in orbital environment
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Johnson, J. D.. 1968-01-01. Techniques developed to determine aerodynamic coefficients for Apollo applications program vehicles in an orbital environment. https://ntrs.nasa.gov/citations/19690023917
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