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Static Aerodynamic Characeristics Of A Winged Single Stage To Orbit Vehicle At Mach Numbers From 03 To 463
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Book Synopsis Static aerodynamic characteristics of a winged single-stage-to-orbit vehicle at Mach numbers from 0.3 to 4.63 by : Delma C. Freeman
Download or read book Static aerodynamic characteristics of a winged single-stage-to-orbit vehicle at Mach numbers from 0.3 to 4.63 written by Delma C. Freeman and published by . This book was released on 1978 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of a Winged Single-stage-to-orbit Vehicle at Mach Numbers from 0.3 to 4.63 by :
Download or read book Static Aerodynamic Characteristics of a Winged Single-stage-to-orbit Vehicle at Mach Numbers from 0.3 to 4.63 written by and published by . This book was released on 1978 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of a Single-stage-to-orbit Vehicle with Low Planform Loading at Mach Numbers from 0.3 to 4.63 by : Delma C. Freeman
Download or read book Static Aerodynamic Characteristics of a Single-stage-to-orbit Vehicle with Low Planform Loading at Mach Numbers from 0.3 to 4.63 written by Delma C. Freeman and published by . This book was released on 1977 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characeristics of a Winged Single-stage-to-orbit Vehicle at Mach Numbers from 0.3 to 4.63 by : Delma C. Freeman
Download or read book Static Aerodynamic Characeristics of a Winged Single-stage-to-orbit Vehicle at Mach Numbers from 0.3 to 4.63 written by Delma C. Freeman and published by . This book was released on 1978 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63 by : Delma C. Freeman
Download or read book Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63 written by Delma C. Freeman and published by . This book was released on 1977 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Modifications on Aerodynamic Characteristics of a Single-stage-to-orbit Vehicle at Mach 5.9 by : Peter T. Bernot
Download or read book Effect of Modifications on Aerodynamic Characteristics of a Single-stage-to-orbit Vehicle at Mach 5.9 written by Peter T. Bernot and published by . This book was released on 1983 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Two Single-stage-to-orbit Vehicles at Mach 20.3 by : Peter T. Bernot
Download or read book Aerodynamic Characteristics of Two Single-stage-to-orbit Vehicles at Mach 20.3 written by Peter T. Bernot and published by . This book was released on 1977 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Data of Space Vehicles by : Claus Weiland
Download or read book Aerodynamic Data of Space Vehicles written by Claus Weiland and published by Springer Science & Business Media. This book was released on 2014-02-22 with total page 360 pages. Available in PDF, EPUB and Kindle. Book excerpt: The capacity and quality of the atmospheric flight performance of space flight vehicles is characterized by their aerodynamic data bases. A complete aerodynamic data base would encompass the coefficients of the static longitudinal and lateral motions and the related dynamic coefficients. In this book the aerodynamics of 27 vehicles are considered. Only a few of them did really fly. Therefore the aerodynamic data bases are often not complete, in particular when the projects or programs were more or less abruptly stopped, often due to political decisions. Configurational design studies or the development of demonstrators usually happen with reduced or incomplete aerodynamic data sets. Therefore some data sets base just on the application of one of the following tools: semi-empirical design methods, wind tunnel tests, numerical simulations. In so far a high percentage of the data presented is incomplete and would have to be verified. Flight mechanics needs the aerodynamic coefficients as function of a lot of variables. The allocation of the aerodynamic coefficients for a particular flight operation at a specific trajectory point is conducted by an aerodynamic model. The establishment of such models is described in this book. This book is written for graduate and doctoral students to give them insight into the aerodynamics of the various flight configurations. Further for design and development engineers in industry and at research institutes (including universities) searching for an appropriate vehicle shape, as well as for non-specialists, who may be interested in this subject. The book will be helpful, too, in the case that system studies require in their concept phases the selection of suitable vehicle shapes.
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781726001076 Total Pages :38 pages Book Rating :4.0/5 (1 download)
Book Synopsis Aerodynamic Characteristics of Two Single-Stage-To-Orbit Vehicles at Mach 20.3 by : National Aeronautics and Space Administration (NASA)
Download or read book Aerodynamic Characteristics of Two Single-Stage-To-Orbit Vehicles at Mach 20.3 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-22 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: The hypersonic stability, control, and performance characteristics of two configurations have been determined. Each configuration had a 50 deg swept delta wing, a vertical tail, and a body flap. One model represented a control configured vehicle with a reduced level of longitudinal static stability; the other model was designed for a conventional level of stability. Data were obtained over an angle of attack range of 0 deg to 50 deg and included effects of component buildup. In addition, the effects of the vertical tail on the lateral directional characteristics were obtained. Bernot, P. T. Langley Research Center NASA-TM-X-3550, L-11627 RTOP 506-26-10-08...
Book Synopsis Aerodynamic Characteristics of Several Proposed Versions of the Saturn V Launch Vehicle at Mach Numbers 1.57 to 4.65 by : Dennis E. Fuller
Download or read book Aerodynamic Characteristics of Several Proposed Versions of the Saturn V Launch Vehicle at Mach Numbers 1.57 to 4.65 written by Dennis E. Fuller and published by . This book was released on 1964 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability and Control Characteristics of a Proposed Winged Reentry Vehicle at Mach Numbers of 1.50, 2.96, and 4.63 by :
Download or read book Static Stability and Control Characteristics of a Proposed Winged Reentry Vehicle at Mach Numbers of 1.50, 2.96, and 4.63 written by and published by . This book was released on 1962 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Relaxed Static Longitudinal Stability on a Single-stage-to-orbit Vehicle Design by : Delma C. Freeman
Download or read book Effects of Relaxed Static Longitudinal Stability on a Single-stage-to-orbit Vehicle Design written by Delma C. Freeman and published by . This book was released on 1979 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Aerodynamic Characteristics of Several Configurations Used in the Development of the Little Joe II-Apollo Test Vehicle at Mach Numbers from 0.056 to 4.65 by : Robert H. Moore
Download or read book Static Longitudinal Aerodynamic Characteristics of Several Configurations Used in the Development of the Little Joe II-Apollo Test Vehicle at Mach Numbers from 0.056 to 4.65 written by Robert H. Moore and published by . This book was released on 1968 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of a Model of a Horizontal-take-off Reusable Launch Vehicle at Mach Numbers 1.60, 2.16, and 2.86 by :
Download or read book Static Aerodynamic Characteristics of a Model of a Horizontal-take-off Reusable Launch Vehicle at Mach Numbers 1.60, 2.16, and 2.86 written by and published by . This book was released on 1965 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability Investigations of Proposed Project Fire Space-vehicle and Reentry-package Configurations at Mach Numbers from 1.47 to 4.63 by : Dennis E. Fuller
Download or read book Static Stability Investigations of Proposed Project Fire Space-vehicle and Reentry-package Configurations at Mach Numbers from 1.47 to 4.63 written by Dennis E. Fuller and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Aerodynamic Characteristics of a 0.028 Scale Model of a Proposed Little Joe-Apollo Space Vehicle at Mach Numbers from 1.50 to 2.16 by :
Download or read book Static Longitudinal Aerodynamic Characteristics of a 0.028 Scale Model of a Proposed Little Joe-Apollo Space Vehicle at Mach Numbers from 1.50 to 2.16 written by and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at Mach Numbers from 0.60 to 1.20 of the Static Aerodynamic Characteristics of a Model of a Possible Nonlifting Reentry Capsule in Combination with a Rocket Booster by : Albin O. Pearson
Download or read book Wind-tunnel Investigation at Mach Numbers from 0.60 to 1.20 of the Static Aerodynamic Characteristics of a Model of a Possible Nonlifting Reentry Capsule in Combination with a Rocket Booster written by Albin O. Pearson and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
