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Longitudinal Stability and Control, Roll Control and Hinge Moments of a Little Joe 2-Apollo Model at Mach Numbers Up to 1.20
Language: en
Pages: 78

Longitudinal Stability and Control, Roll Control and Hinge Moments of a Little Joe 2-Apollo Model at Mach Numbers Up to 1.20

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Type: BOOK - Published: 1964 - Publisher:

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Static Stability and Control Characteristics of a Half-cone Entry Configuration at Mach Numbers from 2.2 to 0.7
Language: en
Pages: 68

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

Authors: Ralph W. Holtzclaw
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Type: BOOK - Published: 1962 - Publisher:

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Stability and Control Characteristics of a Low-lift-drag-ratio Reentry Vehicle at Mach Numbers from 2.30 to 4.65
Language: en
Pages: 28

Stability and Control Characteristics of a Low-lift-drag-ratio Reentry Vehicle at Mach Numbers from 2.30 to 4.65

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Type: BOOK - Published: 1963 - Publisher:

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Static Longitudinal Stability and Control Characteristics at Mach Numbers of 2.86 and 6.02 and Angles of Attack Up to 95 Deg of a Lenticular-shaped Reentry Vehicle
Language: en
Pages: 28

Static Longitudinal Stability and Control Characteristics at Mach Numbers of 2.86 and 6.02 and Angles of Attack Up to 95 Deg of a Lenticular-shaped Reentry Vehicle

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Type: BOOK - Published: 1961 - Publisher:

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Longitudinal Stability and Control Characteristics at Mach Numbers from 0.70 to 2.22 of a Triangular Wing Configuration Equipped with a Canard Control, a Trailing-edge-flap Control, Or a Cambered Forebody
Language: en
Pages: 36

Longitudinal Stability and Control Characteristics at Mach Numbers from 0.70 to 2.22 of a Triangular Wing Configuration Equipped with a Canard Control, a Trailing-edge-flap Control, Or a Cambered Forebody

Authors: John W. Boyd
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Type: BOOK - Published: 1959 - Publisher:

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