Author: Robert M. Lust
Publisher:
ISBN:
Category :
Languages : en
Pages : 50
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 and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87
Author: Donald T. Gregory
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 36
Book Description
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
Author: Marvin Rubinstein
Publisher:
ISBN:
Category : Air-to-air missiles
Languages : en
Pages : 96
Book Description
Publisher:
ISBN:
Category : Air-to-air missiles
Languages : en
Pages : 96
Book Description
Longitudinal Stability Characteristics and Pressure Distribution for a Model of a Long Range Ballistic Missile at Mach Numbers from 0.60 to 3.52
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
Author: Ross B. Robinson
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 32
Book Description
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 Investigation of the Static Stability and Control Characteristics of Winged and Wingless Interceptor Missile Models
Static Stability and Drag Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0
Author: J. T. Best (Jr.)
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 194
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.
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 194
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.
Investigation of the Static Longitudinal Stability Characteristics of an Air-to-surface Canard Missile Configuration in the Transonic Mach Number Range
Author: Gerald L. Hunt
Publisher:
ISBN:
Category : Air-to-surface missiles
Languages : en
Pages : 24
Book Description
Publisher:
ISBN:
Category : Air-to-surface missiles
Languages : en
Pages : 24
Book Description