Author: John T. SuttlesPublisher:
ISBN:
Category : Noses (Space vehicles)
Languages : en
Pages : 70
Book Description
Aerodynamic Characteristics from Mach 0.22 to 4.65 of a Two-stage Rocket Vehicle Having an Unusual Nose Shape
Author: John T. SuttlesPublisher:
ISBN:
Category : Noses (Space vehicles)
Languages : en
Pages : 70
Book Description
Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63
Author: Clarence A. BrownPublisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 86
Book Description
Static Aerodynamic Characteristics of Three Rocket-vehicle Configurations at Mach Numbers from 1.80 to 4.63 Including Some Effects of Fin Size, Fin Cant, and Auxiliary Rocket Motors
Author: Dennis E. FullerPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 64
Book Description
Aerodynamic Characteristics in Pitch of a 1/7-scale Model of a Two- and Three-stage Rocket Configuration at Mach Numbers of 0.4 to 4.63
Author: William F. HinsonPublisher:
ISBN:
Category : Pitching (Aerodynamics)
Languages : en
Pages : 52
Book Description
Aerodynamic characteristics in pitch of scale model of two and three stage rocket configuration at Mach numbers of 0.4 to 4.63.
Aerodynamic Characteristics at a Mach Number of 3.10 of Several Fourth-stage Shapes of the Scout Research Vehicle
Author: Byron M. JaquetPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 22
Book Description
Investigation of the Aerodynamic Characteristics of Two Preliminary Designs of Scout Research Vehicle at Mach Numbers from 1.77 to 4.65
Author: Robert J. KeyntonPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 64
Book Description
Static Aerodynamic Characteristics of a Three-stage Rocket Vehicle Having Various Fin Configurations at Low Subsonic Mach Numbers and Angles of Attack Up to 28 ̊
Author: Clarence A. BrownPublisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 40
Book Description
Effect of First-stage Geometry on Aerodynamic Characteristics in Pitch of Two-stage Rocket Vehicles from Mach 1.57 to 2.86
Author: William A. CorlettPublisher:
ISBN:
Category : Launch vehicles (Astronautics)
Languages : en
Pages : 106
Book Description
Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.16 of a Blunt-nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins
Author: William J. MontaPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36
Book Description
Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63
Author: CLARENCE A. JR. BROWNPublisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
An investigation was conducted in the Langley Unitary Plan wind tunnel to determine the effects of fin cant and size on the static aerodynamic characteristics of a 0.081-scale model of a three-stage and a two-stage Trailblazer II configuration. Tests were performed at Mach numbers from 1.47 to 4.63 and at a Reynolds number per foot of 3.0 x 10 to the 6th power. he angleof-attack range varied from approximately -5 to 5 degrees and angle of sideslip varied from approximately -4 to 4 degrees. All first-stage fins tested gave adequate static stability when the center-of-gravity travel of the flight model was taken into account. The presence of the auxiliary rocket motors in the lateral plane decreased the effectiveness of the fins in the pitch plane at the lower Mach number and increased the fin effectiveness at the higher Mach numbers. Removal of the auxiliary rocket motors from the first stage of the two-stage configuration reduced the axial force about 25% at the low Mach numbers and about 15% at the high Mach numbers. (Author).