Download or read book Space Shuttle Orbiter Trimmed Center of gravity Extension Study Volume 8 Effects of Configuration Modifications on the Aerodynamic Characteristics of the 140 A B Orbiter at a Mach Number of 5 97 written by and published by . This book was released on 1984 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Space Shuttle Orbiter Trimmed Center of gravity Extension Study Volume 9 Effects of Configuration Modifications on the Aerodynamic Characteristics of the 140 A B Orbiter at Mach Numbers of 1 5 2 0 and 2 5 written by and published by . This book was released on 1985 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Space Shuttle Orbiter Trimmed Center of gravity Extension Study Volume 5 Effects of Configuration Modifications on the Aerodynamic Characteristics of the 140A B Orbiter at Mach Numbers of 2 5 3 95 and 4 6 written by and published by . This book was released on 1979 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Space Shuttle Orbiter Trimmed Center of Gravity Extension Study Volume 1 Effects of Configuration Modifications on the Aerodynamic Characteristics of the 140 A B Orbiter at Mach 10 3 written by and published by . This book was released on 1975 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Space Shuttle Orbiter Trimmed Center of gravity Extension Study Volume 2 Effects of Configuration Modifications on the Aerodynamic Characteristics of the 140 A B Orbiter at Transonic Speeds written by and published by . This book was released on 1976 with total page 284 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Space shuttle orbiter trimmed center of gravity extension study written by W. Pelham Phillips and published by . This book was released on 1985 with total page 97 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Space Shuttle Orbiter Trimmed Center of gravity Extension Study written by William I. Scallion and published by . This book was released on 1985 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Space Shuttle Orbiter Trimmed Center of gravity Extension Study Volume 4 Effects of Configuration Modifications on the Aerodynamic Characteristics of the 139B Orbiter at Mach 20 3 written by and published by . This book was released on 1978 with total page 142 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Space Shuttle Orbiter Trimmed Center of gravity Extension Study Volume 7 Effects of Configuration Modifications on the Subsonic Aerodynamic Characteristics of the 1140 A B Orbbiter at High Reynolds Numbers written by and published by . This book was released on 1981 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Space Shuttle Orbiter Trimmed Center of gravity Extension Study Volume 6 System Design Studies written by and published by . This book was released on 1978 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Space Shuttle Orbiter Trimmed Center of gravity Extension Study written by William I. Scallion and published by . This book was released on 1985 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Space Shuttle Orbiter Trimmed Center of gravity Extension Study Volume 3 Impact of Retrofits for Center of gravity Extension on Orbiter Thermal protection System written by and published by . This book was released on 1979 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Space Shuttle Orbiter Trimmed Center Of Gravity Extension Study Volume 6 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-13 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: System studies were made to determine the required changes in shuttle orbiter mass for various changes in aerodynamic shape. These changes are designed to extend the current shuttle orbiter trimmed c.g. envelope to accommodate a greater range of payloads. One of the apparently most viable changes for the amount of c.g. extension obtained involves the removal of the present wing/body fillet and the replacement of this structural element with a forward located fixed canard. Macconochie, I. O. Langley Research Center NASA-TM-72661-VOL-6 RTOP 506-26-30-04...
Download or read book Aerodynamic Characteristics of the 140A B Space Shuttle Orbiter at Mach 10 3 written by Peter T. Bernot and published by . This book was released on 1979 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic longitudinal aerodynamic characteristics of two space shuttle orbiter configurations written by James C. Ellison and published by . This book was released on 1977 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Effects of Lateral Aerodynamic Uncertainties on the Handling Qualities of the Space Shuttle Orbiter at Mach Numbers of 1 5 and 6 written by and published by . This book was released on 1981 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Reynolds Number and Body Corner Radius on Aerodynamic Characteristics of a Space Shuttle type Vehicle at Subsonic Mach Numbers written by Leland Howard Jorgenson and published by . This book was released on 1972 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Static aerodynamic forces and moments were measured to study the effects of Reynolds number and body corner radius on the aerodynamic characteristics of a straight wing space shuttle orbiter at subsonic speeds. A 0.02-scale model was tested at Mach numbers from 0.3 to 0.9 and Reynolds numbers from about 600,000 to 3 million, based on body width. The body alone and the body with its wing and horizontal tail attached were tested at angles of attack from 35 to 75 degrees. The effects of rounding the body corners at the junctures connecting the bottom and sides were investigated for corner radii from 0 to 8.5 percent of the body width. At low subsonic Mach numbers (free stream Mach number approximately equal 0.3) the aerodynamic characteristics are affected significantly by changes in Reynolds number and body corner radius. With increase in Mach number to free stream Mach number = 0.9 the effect of Reynolds number seems to vanish, but a significant effect of body corner radius remains.
