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

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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Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63
Language: en
Pages: 86
Authors: Clarence A. Brown
Categories: Space vehicles
Type: BOOK - Published: 1962 - Publisher:

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Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63
Language: en
Pages: 1
Authors: CLARENCE A. JR. BROWN
Categories:
Type: BOOK - Published: 1962 - Publisher:

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An investigation was conducted in the Langley Unitary Plan wind tunnel to determine the effects of fin cant and size on the static aerodynamic characteristics o
Static Aerodynamic Characteristics of a Three-stage Rocket Vehicle Having Various Fin Configurations at Low Subsonic Mach Numbers and Angles of Attack Up to 28 ̊
Language: en
Pages: 40