The Aerodynamic Characteristics of a Blunt Half Cone Entry Configurations Obtained from Ballistic Range Tests at Mach Numbers Near 3

The Aerodynamic Characteristics of a Blunt Half Cone Entry Configurations Obtained from Ballistic Range Tests at Mach Numbers Near 3 PDF Author:
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Languages : en
Pages : 38

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Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers of 5.2, 7.4, and 10.4

Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers of 5.2, 7.4, and 10.4 PDF Author:
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Languages : en
Pages : 78

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Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers from 10.9 to 21.2 in Helium

Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers from 10.9 to 21.2 in Helium PDF Author:
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Languages : en
Pages : 96

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NASA Technical Note

NASA Technical Note PDF Author:
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Languages : en
Pages : 616

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Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers from 3 to 6

Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers from 3 to 6 PDF Author: Michael F. Sarabia
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Languages : en
Pages : 44

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Large-scale Wind-tunnel Investigation of an M1-L Lifting Body with an Inflatable and a Rigid Afterbody

Large-scale Wind-tunnel Investigation of an M1-L Lifting Body with an Inflatable and a Rigid Afterbody PDF Author: Kenneth W. Mort
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Category : Aerodynamics
Languages : en
Pages : 36

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Static Stability and Control Characteristics of a Half-cone Entry Configuration at Mach Numbers from 2.2 to 0.7

Static Stability and Control Characteristics of a Half-cone Entry Configuration at Mach Numbers from 2.2 to 0.7 PDF Author: Ralph W. Holtzclaw
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Languages : en
Pages : 68

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The Static and Dynamic Stability Derivatives of a Blunt Half-cone Entry Configuration at Mach Numbers from 0.70 to 3.50

The Static and Dynamic Stability Derivatives of a Blunt Half-cone Entry Configuration at Mach Numbers from 0.70 to 3.50 PDF Author:
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Languages : en
Pages : 42

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Aerodynamic Characteristics of Two Blunt, Half-cone Wedge Entry Configurations at Mach Numbers from 2.30 to 4.63

Aerodynamic Characteristics of Two Blunt, Half-cone Wedge Entry Configurations at Mach Numbers from 2.30 to 4.63 PDF Author: Gerald V. Foster
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Languages : en
Pages : 33

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Aerodynamic Characteristics of a Blunt, Half-cone Entry Configuration, with Horizontal Landing Capability

Aerodynamic Characteristics of a Blunt, Half-cone Entry Configuration, with Horizontal Landing Capability PDF Author:
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Languages : en
Pages : 30

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