Author: C. Donald Babb
Publisher:
ISBN:
Category : Sounding rockets
Languages : en
Pages : 82
Book Description
Static Stability Investigation of a Sounding-rocket Vehicle at Mach Numbers from 1.50 to 4.63
Author: C. Donald Babb
Publisher:
ISBN:
Category : Sounding rockets
Languages : en
Pages : 82
Book Description
Publisher:
ISBN:
Category : Sounding rockets
Languages : en
Pages : 82
Book Description
Static Stability Investigation of a Sounding-rocket Vehicle at Mach Numbers from 1.50 to 4.63
Static Stability Investigation of a Single-stage Sounding Rocket at Mach Numbers from 0.60 to 1.20
Author: James C. Ferris
Publisher:
ISBN:
Category : Sounding rockets
Languages : en
Pages : 68
Book Description
Publisher:
ISBN:
Category : Sounding rockets
Languages : en
Pages : 68
Book Description
Static Stability Investigation of a Single-stage Sounding Rocket at Mach Numbers from 0.60 to 1.20
Statistic Stability Investigation of a Single-stage Sounding Rocket at Mach Numbers from 0.60 to 1.20
Static Stability Investigations of Proposed Project Fire Space-vehicle and Reentry-package Configurations at Mach Numbers from 1.47 to 4.63
Author: Dennis E. Fuller
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 28
Book Description
Investigation of the Static Stability Characteristics of a Reentry Spacecraft Model in Free Flight for Mach Numbers from 2.62 to 1.11 Launched at an Angle of Attack of 180°
Author: J. W. Usry
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
Static Stability and Separation Characteristics of a Two-stage Rocket Configuration at Mach Numbers from 1.57 to 4.50
Author: Kenneth L. Turner
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
Book Description
Static Aerodynamic Characteristics of a Rocket Vehicle with Thick Wedge Fins and Sweptback Leading and Trailing Edges
Author: Joseph A. Yuska
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 20
Book Description
The longitudinal static stability characteristics of three one-fifth scale models of the second stage of a sounding rocket were calculated and compared with the measured values at Mach numbers of 1.79 to 3.47. All three models had fins of trapezoidal planform with sweptback leading and trailing edges, small aspect ratio, and thick wedge sections, but differed in fin area and overall model length. Calculation of center of pressure and normal-force coefficient slope at zero normal force were in good agreement with experimental data.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 20
Book Description
The longitudinal static stability characteristics of three one-fifth scale models of the second stage of a sounding rocket were calculated and compared with the measured values at Mach numbers of 1.79 to 3.47. All three models had fins of trapezoidal planform with sweptback leading and trailing edges, small aspect ratio, and thick wedge sections, but differed in fin area and overall model length. Calculation of center of pressure and normal-force coefficient slope at zero normal force were in good agreement with experimental data.