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 PDF Author: Clarence A. Brown
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ISBN:
Category : Space vehicles
Languages : en
Pages : 86

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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

Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63 PDF Author: Clarence A. Brown
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 86

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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

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 PDF Author: Dennis E. Fuller
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ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 64

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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

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 PDF Author: William F. Hinson
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ISBN:
Category : Pitching (Aerodynamics)
Languages : en
Pages : 52

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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.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1492

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Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author:
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ISBN:
Category : Science
Languages : en
Pages : 812

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Static Aerodynamic Characteristics of a Single-stage-to-orbit Vehicle with Low Planform Loading at Mach Numbers from 0.3 to 4.63

Static Aerodynamic Characteristics of a Single-stage-to-orbit Vehicle with Low Planform Loading at Mach Numbers from 0.3 to 4.63 PDF Author: Delma C. Freeman
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ISBN:
Category :
Languages : en
Pages : 76

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Supersonic Aerodynamic Characteristics of a 1/6-scale Model of the Final Two Stages of the Argo D-4 Four-stage Rocket Vehicle

Supersonic Aerodynamic Characteristics of a 1/6-scale Model of the Final Two Stages of the Argo D-4 Four-stage Rocket Vehicle PDF Author: Clyde Hayes
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ISBN:
Category :
Languages : en
Pages : 28

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Aerodynamic Loading Characteristics of a 1/10-scale Model of the Three-stage Scout Vehicle at Mach Numbers 1.57 to 4.65

Aerodynamic Loading Characteristics of a 1/10-scale Model of the Three-stage Scout Vehicle at Mach Numbers 1.57 to 4.65 PDF Author: Lloyd S. Jernell
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ISBN:
Category : Aerodynamic load
Languages : en
Pages : 52

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Investigation of the Aerodynamic Characteristics of Two Preliminary Designs of Scout Research Vehicle at Mach Numbers from 1.77 to 4.65

Investigation of the Aerodynamic Characteristics of Two Preliminary Designs of Scout Research Vehicle at Mach Numbers from 1.77 to 4.65 PDF Author: Robert J. Keynton
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ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 64

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Wind-tunnel Investigation at Mach Numbers from 0.30 to 1.20 of the Static Aerodynamic Characteristics of a Two-stage Saturn Launch Vehicle

Wind-tunnel Investigation at Mach Numbers from 0.30 to 1.20 of the Static Aerodynamic Characteristics of a Two-stage Saturn Launch Vehicle PDF Author:
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ISBN:
Category :
Languages : en
Pages : 36

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