Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87 PDF Download

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Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87

Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87 PDF Author: Donald T. Gregory
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 36

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Book Description

Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87

Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87 PDF Author: Donald T. Gregory
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 36

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Book Description

Investigation of the Static Longitudinal Stability Characteristics of an Air-to-surface Canard Missile Configuration in the Transonic Mach Number Range

Investigation of the Static Longitudinal Stability Characteristics of an Air-to-surface Canard Missile Configuration in the Transonic Mach Number Range PDF Author: Gerald L. Hunt
Publisher:
ISBN:
Category : Air-to-surface missiles
Languages : en
Pages : 24

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Investigation of Static Longitudinal Stability and Control Characteristics of a 33 1/3% Scale DR-123 Missile at Mach Numbers 1.61, 2.05, and 2.58

Investigation of Static Longitudinal Stability and Control Characteristics of a 33 1/3% Scale DR-123 Missile at Mach Numbers 1.61, 2.05, and 2.58 PDF Author: Marvin Rubinstein
Publisher:
ISBN:
Category : Air-to-air missiles
Languages : en
Pages : 96

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Static Longitudinal Stability and Control Characteristics at a Mach Number of 2.01 of a Hypersonic Missile Configuration Having All-movable Wing and Tail Surfaces

Static Longitudinal Stability and Control Characteristics at a Mach Number of 2.01 of a Hypersonic Missile Configuration Having All-movable Wing and Tail Surfaces PDF Author: Ross B. Robinson
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 32

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Book Description

Investigation of the Static Longitudinal Stability Characteristics of a Model of an Intermediate-range Ballistic Missile at Mach Numbers Between 1.57 and 4.65

Investigation of the Static Longitudinal Stability Characteristics of a Model of an Intermediate-range Ballistic Missile at Mach Numbers Between 1.57 and 4.65 PDF Author: Robert M. Lust
Publisher:
ISBN:
Category :
Languages : en
Pages : 50

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An Experimental Investigation of the Static Longitudinal Stability and Control Characteristics of a Wingless Missile Configuration at Mach Numbers from 3.0 to 6.3

An Experimental Investigation of the Static Longitudinal Stability and Control Characteristics of a Wingless Missile Configuration at Mach Numbers from 3.0 to 6.3 PDF Author: Hermilo R. Gloria
Publisher:
ISBN:
Category :
Languages : en
Pages : 29

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Book Description

Static Longitudinal Stability and Control Characteristics at a Mach Number of 2.01 of a Hypersonic Missile Configuration Having All-movable Wing and Tail Surfaces

Static Longitudinal Stability and Control Characteristics at a Mach Number of 2.01 of a Hypersonic Missile Configuration Having All-movable Wing and Tail Surfaces PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 32

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Book Description

Investigation of the Static Stability Characteristics of Two Stages of a Three-stage Missile at a Mach Number of 4.00

Investigation of the Static Stability Characteristics of Two Stages of a Three-stage Missile at a Mach Number of 4.00 PDF Author: Ausley B. Carraway
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 18

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Book Description

Static Stability and Drag Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0

Static Stability and Drag Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0 PDF Author: J. T. Best (Jr.)
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 194

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Book Description
Static-force tests were conducted at Mach number 2.25, 3, and 4 on a 0.25 -scale model of the High Altitude Supersonic Target (HAST) missile.

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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Book Description