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Author : Donald L. Edberg,Guillermo Costa,Willie Costa Publisher : American Institute of Aeronautics and Astronautics Incorporated Page : 0 pages File Size : 54,9 Mb Release : 2020 Category : Launch vehicles (Astronautics) ISBN : 1624105939
Design of Rockets and Space Launch Vehicles by Donald L. Edberg,Guillermo Costa,Willie Costa Pdf
With growing interest in space activity and numerous new launchers in development, this book is a timely, comprehensive survey of important concepts and applications. It enhances understanding and provides exposure to practical aspects of design, manufacturing, testing, and engineering associated with these topics.
Design of Rockets and Space Launch Vehicles by Donald L. Edberg,Guillermo Costa Pdf
"Interest is growing in space activity, and many new launchers are in development. Design of Rockets and Space Launch Vehicles, Second Edition is a timely and comprehensive exposé of important concepts and applications. This newly updated edition provides enhanced understanding and exposure to the latest developments in the practical aspects of design, engineering, manufacturing, and testing. Although it is primarily intended for readers with at least a 3rd-year level knowledge of aerospace engineering, mathematics, and physics, because it contains many applications and step-by-step illustrated examples along with photographs or line drawings of actual hardware, it will also be of interest to practicing engineers, technical managers, and others who are interested in "how rockets work" in either the "big picture" sense, or in areas other than one's specialty. This book will answer many questions as to "why things are done this way.""--
Annotation This practical book gives young professionals all the information they need to know to get started in the space business. It takes you step-by-step through processes for systems engineering and acquisition, design and development, cost analysis, and program planning and analysis. You'll find the systems engineering and design process that applies to all space transportation systems, then the overall system architecture considerations that also apply to all space transportation systems. There is also detailed coverage of space launch vehicles by class, including the current space shuttle, other manned reusable systems, expendable systems, and future systems. A companion CD-ROM contains the Operations Simulation and Analysis Modeling System software.
Since ancient times, men and women have dreamed of soaring among the stars, but only in this century has that dream been realized. In Rockets into Space, Frank Winter tells the fascinating story of the modern launch vehicle, from the mythological musings of the Babylonians and Greeks to the present-day reality of manned and unmanned space flight. In concise yet comprehensive chapters dense with anecdotal detail, Winter tracks the theoretical formulations and technological breakthroughs that have charted the evolution of rocket propulsion and vehicle design. He pays particular attention to the remarkable contributions of pioneers Konstantin Tsiolkovsky, Robert Goddard, Hermann Oberth, Eugen Sänger, and Sergei Korolev, whose genius and vision paved the way for later innovation. He describes the clandestine development of the V-2 rocket in Germany, under the technical leadership of Wernher von Braun, and its dramatic impact on postwar rocket research and satellite development in the United States and the Soviet Union. He also chronicles the complex events of the last three decades, which have produced ever more sophisticated rockets capable of launching larger payloads, from weapons to weather and communications satellites. Finally, he surveys exotic propulsion systems--nuclear, electric, solar, photon, laser--that lie on the frontiers of science today but that will shape the spaceflight and space policy decisions of tomorrow. Rockets into Space is an authoritative, entertaining guidebook for all who are interested in the history of space travel.
The Development of Propulsion Technology for U.S. Space-Launch Vehicles, 1926-1991 by J. D. Hunley Pdf
In this definitive study, J. D. Hunley traces the program’s development from Goddard’s early rockets (and the German V-2 missile) through the Titan IVA and the Space Shuttle, with a focus on space-launch vehicles. Since these rockets often evolved from early missiles, he pays considerable attention to missile technology, not as an end in itself, but as a contributor to launch-vehicle technology. Focusing especially on the engineering culture of the program, Hunley communicates this very human side of technological development by means of anecdotes, character sketches, and case studies of problems faced by rocket engineers. He shows how such a highly adaptive approach enabled the evolution of a hugely complicated technology that was impressive—but decidedly not rocket science. Unique in its single-volume coverage of the evolution of launch-vehicle technology from 1926 to 1991, this meticulously researched work will inform scholars and engineers interested in the history of technology and innovation, as well as those specializing in the history of space flight.
This book describes a new type of rocket science needed to create low-cost, reliable, responsive space transportation. You don't have to be a rocket scientist to understand the issues explored within this book. The text is beyond the current state-of-the-art engineering of modern launch vehicles, going into a scientific investigation that opens the door to true design optimization. The purpose of this work is to enable the reader to understand how low-cost space transportation is practical, and why it has been so hard to achieve.
Dynamics and Simulation of Flexible Rockets by Timothy M. Barrows,Jeb S. Orr Pdf
Dynamics and Simulation of Flexible Rockets provides a full state, multiaxis treatment of launch vehicle flight mechanics and provides the state equations in a format that can be readily coded into a simulation environment. Various forms of the mass matrix for the vehicle dynamics are presented. The book also discusses important forms of coupling, such as between the nozzle motions and the flexible body. This book is designed to help practicing aerospace engineers create simulations that can accurately verify that a space launch vehicle will successfully perform its mission. Much of the open literature on rocket dynamics is based on analysis techniques developed during the Apollo program of the 1960s. Since that time, large-scale computational analysis techniques and improved methods for generating Finite Element Models (FEMs) have been developed. The art of the problem is to combine the FEM with dynamic models of separate elements such as sloshing fuel and moveable engine nozzles. The pitfalls that may occur when making this marriage are examined in detail. Covers everything the dynamics and control engineer needs to analyze or improve the design of flexible launch vehicles Provides derivations using Lagrange’s equation and Newton/Euler approaches, allowing the reader to assess the importance of nonlinear terms Details the development of linear models and introduces frequency-domain stability analysis techniques Presents practical methods for transitioning between finite element models, incorporating actuator dynamics, and developing a preliminary flight control design
Design of an Airborne Launch Vehicle for an Air Launched Space Booster by National Aeronautics and Space Administration (NASA) Pdf
A conceptual design is presented for a carrier vehicle for an air launched space booster. This airplane is capable of carrying a 500,000 pound satellite launch system to an altitude over 40,000 feet for launch. The airplane features a twin fuselage configuration for improved payload and landing gear integration, a high aspect ratio wing for maneuverability at altitude, and is powered by six General Electric GE-90 engines. The analysis methods used and the systems employed in the airplane are discussed. Launch costs are expected to be competitive with existing launch systems. Chao, Chin and Choi, Rich and Cohen, Scott and Dumont, Brian and Gibin, Mauricius and Jorden, Rob and Poth, Stefan Unspecified Center AIR LAUNCHING; AIRCRAFT DESIGN; BOOSTER ROCKETS; EDUCATION; LAUNCH VEHICLES; OPERATING COSTS; SPACECRAFT LAUNCHING; STUDENTS; UNIVERSITY PROGRAM; FUSELAGES; LANDING GEAR; MANEUVERABILITY; PAYLOAD INTEGRATION; SLENDER WINGS; UNIVERSITIES...
International Reference Guide to Space Launch Systems by Steven J. Isakowitz,Joseph P. Hopkins,Joshua B. Hopkins Pdf
This bestselling reference guide contains the most reliable and comprehensive material on launch programs in Brazil, China, Europe, India, Israel, and the United States. Packed with illustrations and figures, this edition has been updated and expanded, and offers a quick and easy data retrieval source for policy makers, planners, engineers, launch buyers, and students.
Elements of Spacecraft Design by Charles D. Brown Pdf
Annotation This text discusses the conceptual stages of mission design, systems engineering, and orbital mechanics, providing a basis for understanding the design process for different components and functions of a spacecraft. Coverage includes propulsion and power systems, structures, attitude control, thermal control, command and data systems, and telecommunications. Worked examples and exercises are included, in addition to appendices on acronyms and abbreviations and spacecraft design data. The book can be used for self-study or for a course in spacecraft design. Brown directed the team that produced the Magellan spacecraft, and has taught spacecraft design at the University of Colorado. Annotation c. Book News, Inc., Portland, OR (booknews.com).
National Security Space Launch Report by Forrest McCartney Pdf
In 1994, the National Space Transportation Policy laid the framework for appropriate government agencies to maintain strong launch systems and infrastructure while modernizing space transportation capabilities and encouraging cost reductions. More than a decade later, through combined Department of Defense (DoD) and industrial investment, the two Evolved Expendable Launch Vehicle (EELV) families of U.S. rockets (Atlas V and Delta IV) have proved to be maturing, reliable state-of-the-art technologies. In 2004, Congress directed the Secretary of Defense to establish a panel of experts with extensive space launch and operations background to address the future National Security Space launch requirements and the means of meeting those requirements. DoD selected RAND to facilitate and support this panel in its deliberations between May 2005 and May 2006. This report analyzes the National Security Space (NSS) Launch Requirements Panel's major findings and recommendations. In short, the Panel concludes that, because basic rocketry principles, use of chemically derived thrust, and multiple expendable stages seem certain to remain the design of choice for operational space launch vehicles, the EELV can satisfy all known and projected NSS requirements through 2020.
National Research Council,Division on Engineering and Physical Sciences,Air Force Science and Technology Board,Committee on the National Aerospace Initiative
Author : National Research Council,Division on Engineering and Physical Sciences,Air Force Science and Technology Board,Committee on the National Aerospace Initiative Publisher : National Academies Press Page : 146 pages File Size : 55,7 Mb Release : 2004-06-16 Category : Science ISBN : 9780309166126
Evaluation of the National Aerospace Initiative by National Research Council,Division on Engineering and Physical Sciences,Air Force Science and Technology Board,Committee on the National Aerospace Initiative Pdf
The National Aerospace Initiative (NAI) was conceived as a joint effort between the Department of Defense (DOD) and the National Aeronautics and Space Administration (NASA) to sustain the aerospace leadership of the United States through the acceleration of selected aerospace technologies: hypersonic flight, access to space, and space technologies. The Air Force became concerned about the NAI's possible consequences on Air Force programs and budget if NAI program decisions differed from Air Force priorities. To examine this issue, it asked the NRC for an independent review of the NAI. This report presents the results of that assessment. It focuses on three questions asked by the Air Force: is NAI technically feasible in the time frame laid out; is it financially feasible over that period; and is it operationally relevant.
National Research Council,Division on Engineering and Physical Sciences,Aeronautics and Space Engineering Board,Committee for the Reusable Booster System: Review and Assessment
Author : National Research Council,Division on Engineering and Physical Sciences,Aeronautics and Space Engineering Board,Committee for the Reusable Booster System: Review and Assessment Publisher : National Academies Press Page : 115 pages File Size : 54,6 Mb Release : 2013-01-10 Category : Science ISBN : 9780309266567
Reusable Booster System by National Research Council,Division on Engineering and Physical Sciences,Aeronautics and Space Engineering Board,Committee for the Reusable Booster System: Review and Assessment Pdf
On June 15, 2011, the Air Force Space Command established a new vision, mission, and set of goals to ensure continued U.S. dominance in space and cyberspace mission areas. Subsequently, and in coordination with the Air Force Research Laboratory, the Space and Missile Systems Center, and the 14th and 24th Air Forces, the Air Force Space Command identified four long-term science and technology (S&T) challenges critical to meeting these goals. One of these challenges is to provide full-spectrum launch capability at dramatically lower cost, and a reusable booster system (RBS) has been proposed as an approach to meet this challenge. The Air Force Space Command asked the Aeronautics and Space Engineering Board of the National Research Council to conduct an independent review and assessment of the RBS concept prior to considering a continuation of RBS-related activities within the Air Force Research Laboratory portfolio and before initiating a more extensive RBS development program. The committee for the Reusable Booster System: Review and Assessment was formed in response to that request and charged with reviewing and assessing the criteria and assumptions used in the current RBS plans, the cost model methodologies used to fame [frame?] the RBS business case, and the technical maturity and development plans of key elements critical to RBS implementation. The committee consisted of experts not connected with current RBS activities who have significant expertise in launch vehicle design and operation, research and technology development and implementation, space system operations, and cost analysis. The committee solicited and received input on the Air Force launch requirements, the baseline RBS concept, cost models and assessment, and technology readiness. The committee also received input from industry associated with RBS concept, industry independent of the RBS concept, and propulsion system providers which is summarized in Reusable Booster System: Review and Assessment.
