Re Entry And Vehicle Design
Download Re Entry And Vehicle Design full books in PDF, epub, and Kindle. Read online free Re Entry And Vehicle Design ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Author | : Patrick Gallais |
Publisher | : Springer Science & Business Media |
Total Pages | : 365 |
Release | : 2007-09-23 |
Genre | : Technology & Engineering |
ISBN | : 3540736476 |
Based on a long engineering experience, this book offers a comprehensive and state-of-the-art analysis of aerodynamic and flight mechanic entry topics. This updated edition had new chapters on Re-entry on Mars mission, flight quality, rarefied aerodynamics and re-entry accuracy. In addition, it provides a large set of application exercises and solutions.
Author | : Donald P. Legalley |
Publisher | : Academic Press |
Total Pages | : 433 |
Release | : 2014-05-12 |
Genre | : Technology & Engineering |
ISBN | : 1483270823 |
Ballistic Missile and Space Technology, Volume IV: Re-Entry and Vehicle Design focuses on the advancements of processes, methodologies, and technologies involved in re-entry and vehicle design, including hypersonics, material structures, propulsion, and communications. The selection first offers information on the pyrolysis of plastics in a high vacuum arc image furnace and aerothermodynamic feasibility of graphite for hypersonic glide vehicles. Discussions focus on aerothermochemical behavior of graphite, transient heat conduction, equilibrium glide trajectory, and apparatus and pyrolysis procedure. The text then takes a look at an engineering analysis of the weights of ablating systems for manned reentry vehicles and trajectories of lifting bodies entering planetary atmospheres at shallow angles. The manuscript ponders on propulsive control of atmospheric entry lifting trajectories, re-entry engineering mechanics, and rocket casing behavior predicted by laboratory tests. Topics include description of testing program, full-scale casing results, camera design, theoretical correlation, approximate thrust vector optimization, and propellant weight estimation. The selection is a dependable reference for astronauts and researchers interested in re-entry and vehicle design.
Author | : Wilbur L. Hankey |
Publisher | : AIAA |
Total Pages | : 160 |
Release | : 1988 |
Genre | : Space vehicles |
ISBN | : 9781600861062 |
Author | : Michael Douglas Griffin |
Publisher | : AIAA |
Total Pages | : 700 |
Release | : 2004 |
Genre | : Space vehicles |
ISBN | : 9781600861123 |
Author | : Ernst Heinrich Hirschel |
Publisher | : Springer Science & Business Media |
Total Pages | : 512 |
Release | : 2009-11-26 |
Genre | : Technology & Engineering |
ISBN | : 354089974X |
In this book selected aerothermodynamic design problems in hypersonic vehicles are treated. Where applicable, it emphasizes the fact that outer surfaces of hypersonic vehicles primarily are radiation-cooled, an interdisciplinary topic with many implications.
Author | : William Yengst |
Publisher | : Tate Publishing |
Total Pages | : 308 |
Release | : 2010-04 |
Genre | : History |
ISBN | : 1615665471 |
History shows that demands of wartime military and political leaders have often motivated development of new and advanced technologies. The German desire to attack American cities with long-range variants of V-2 missiles during the latter years of World War II stimulated development of maneuvering reentry vehicle concepts. In the mid-1960s, these concepts were secretly refined and tested by the United States to provide accurate delivery of strategic nuclear warheads at intercontinental ranges and to assure their penetration of newly developed Soviet anti-ballistic missile defenses. First Maneuvering Reentry Vehicles, by William C. Yengst, describes the initial feasibility programs to test three alternative designs for implementing hypersonic maneuvers and accurate guidance of long-range reentry vehicles. It identifies the political and military motivations, environmental challenges, design difficulties, innovative technology solutions, test failures, and spectacular successes. It also summarizes development of operational maneuvering reentry vehicles prepared for U.S. Air Force, Navy, and Army long-range missile systems during the 1980s. The technology has been adopted and further refined by foreign nations (India, China and Russia) in building their latest missile systems. Therefore, it is important to understand the capabilities and performance characteristics of future potential threats. Written as a first-hand account of the technology's evolution, the book honors the dedicated engineers and scientists who worked to make these programs a success.
Author | : Frank J. Regan |
Publisher | : AIAA |
Total Pages | : 616 |
Release | : 1993 |
Genre | : Space vehicles |
ISBN | : 9781600860461 |
Author | : Claus Weiland |
Publisher | : Springer Science & Business Media |
Total Pages | : 360 |
Release | : 2014-02-22 |
Genre | : Technology & Engineering |
ISBN | : 3642541682 |
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 | : B.N. Suresh |
Publisher | : Springer |
Total Pages | : 792 |
Release | : 2015-11-20 |
Genre | : Technology & Engineering |
ISBN | : 8132225325 |
The book addresses the overall integrated design aspects of a space transportation system involving several disciplines like propulsion, vehicle structures, aerodynamics, flight mechanics, navigation, guidance and control systems, stage auxiliary systems, thermal systems etc. and discusses the system approach for design, trade off analysis, system life cycle considerations, important aspects in mission management, the risk assessment, etc. There are several books authored to describe the design aspects of various areas, viz., propulsion, aerodynamics, structures, control, etc., but there is no book which presents space transportation system (STS) design in an integrated manner. This book attempts to fill this gap by addressing systems approach for STS design, highlighting the integrated design aspects, interactions between various subsystems and interdependencies. The main focus is towards the complex integrated design to arrive at an optimum, robust and cost effective space transportation system. The orbital mechanics of satellites including different coordinate frames, orbital perturbations and orbital transfers are explained. For launching the satellites to meet specific mission requirements, viz., payload/orbit, design considerations, giving step by step procedure are briefed. The selection methodology for launch vehicle configuration, its optimum staging and the factors which influence the vehicle performance are summarized. The influence of external, internal and dynamic operating environments experienced by the vehicle subsystems and the remedial measures needed are highlighted. The mission design strategies and their influence on the vehicle design process are elaborated. The various critical aspects of STS subsystems like flight mechanics, propulsion, structures and materials, thermal systems, stage auxiliary systems, navigation, guidance and control and the interdependencies and interactions between them are covered. The design guidelines, complexity of the flight environment and the reentry dynamics for the reentry missions are included. The book is not targeted as a design tool for any particular discipline or subsystem. Some of the design related equations or expressions are not attempted to derive from the first principle as this is beyond the scope of this book. However, the important analytical expressions, graphs and sketches which are essential to provide in-depth understanding for the design process as well as to understand the interactions between different subsystems are appropriately included.
Author | : Nguyen Vinh |
Publisher | : Elsevier |
Total Pages | : 421 |
Release | : 2012-12-02 |
Genre | : Technology & Engineering |
ISBN | : 0444601457 |
Optimal Trajectories in Atmospheric Flight deals with the optimization of trajectories in atmospheric flight. The book begins with a simple treatment of functional optimization followed by a discussion of switching theory. It then presents the derivation of the general equations of motion along with the basic knowledge in aerodynamics and propulsion necessary for the analysis of atmospheric flight trajectories. It goes on to the study of optimal trajectories by providing the general properties of the optimal aerodynamic controls and the integrals of motion. This is followed by discussions of high subsonic and supersonic flight, and approximation techniques to reduce the order of the problem for a fast computation of the optimal trajectory. The final chapters present analyses of optimal reentry trajectories and orbital maneuvers. This book is intended as a reference text for scientists and engineers wanting to get into the subject of optimal trajectories in atmospheric flight. If used for teaching purposes, the book is written in a self-contained way so that a selective use of the material is at the discretion of the lecturer. The first 11 chapters are sufficient for a one-semester course with emphasis on optimal maneuvers of high performance aircraft.