Static Aerodynamic Characteristics Of Three Rocket Vehicle Configurations At Mach Numbers From 180 To 463 Including Some Effects Of Fin Size Fin Cant And Auxiliary Rocket Motors
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Static Aerodynamic Characteristics of Three Rocket-vehicle Configurations at Mach Numbers from 1.80 to 4.63 Including Some Effects of Fin Size, Fin Cant, and Auxiliary Rocket Motors
Author | : Dennis E. Fuller |
Publisher | : |
Total Pages | : 64 |
Release | : 1963 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
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