Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63 PDF Download

Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63 PDF full book. Access full book title Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63 by Clarence A. Brown. Download full books in PDF and EPUB format.

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. Brown
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 86

Get Book

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. Brown
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 86

Get Book

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. Fuller
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 64

Get Book

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. Keynton
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 64

Get Book

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. Hinson
Publisher:
ISBN:
Category : Pitching (Aerodynamics)
Languages : en
Pages : 52

Get Book

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 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. Monta
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36

Get Book

Book Description

Supersonic Aerodynamic Characteristics of a 1/6-scale Model of the Final Two Stages of the Argo D-4 Four-stage Rocket Vehicle

Author: Clyde Hayes
Publisher:
ISBN:
Category :
Languages : en
Pages : 28

Get Book

Book Description

Aerodynamic Characteristics Over a Mach Number Range of 1.40 to 2.78 of a Rocket-propelled Airplane Configuration Having a Low 52.2© Delta Wing and an Unswept Horizontal Tail

Author: Alan B. Kehlet
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 30

Get Book

Book Description

Aerodynamic Characteristics Over a Mach Number Range of 1.40 to 2.78 of a Rocket-propelled Airplane Configuration Having a Low 52.20 Delta Wing and an Unswept Horizontal Tail

Author: Alan B. Kehlet
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 30

Get Book

Book Description

Aerodynamic Characteristics of Two Single-stage-to-orbit Vehicles at Mach 20.3

Author: Peter T. Bernot
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 40

Get Book

Book Description

Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63

Author: James F. Campbell
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44

Get Book

Book Description