Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63

Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63
Author: Clarence A. Brown
Publisher:
Total Pages: 86
Release: 1962
Genre: Space vehicles
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
Aerodynamic Characteristics in Pitch of a 1/7-scale Model of a Two- and Three-stage Rocket Configuration at Mach Numbers of 0.4 to 4.63
Language: en
Pages: 52
Authors: William F. Hinson
Categories: Pitching (Aerodynamics)
Type: BOOK - Published: 1969 - Publisher:

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Aerodynamic characteristics in pitch of scale model of two and three stage rocket configuration at Mach numbers of 0.4 to 4.63.