Theory of Aerospace Propulsion

Theory of Aerospace Propulsion
Author: P. M. Sforza
Publsiher: Elsevier
Total Pages: 684
Release: 2011-11-04
ISBN 10: 1856179125
ISBN 13: 9781856179126
Language: EN, FR, DE, ES & NL

Theory of Aerospace Propulsion Book Review:

Readers of this book will be able to: utilize the fundamental principles of fluid mechanics and thermodynamics to analyze aircraft engines, understand the common gas turbine aircraft propulsion systems and be able to determine the applicability of each, perform system studies of aircraft engine systems for specified flight conditions, perform preliminary aerothermal design of turbomachinery components, and conceive, analyze, and optimize competing preliminary designs for conventional and unconventional missions. Early coverage of cycle analysis provides a systems perspective, and offers context for the chapters on turbomachinery and components Broader coverage than found in most other books - including coverage of propellers, nuclear rockets, and space propulsion - allows analysis and design of more types of propulsion systems In depth, quantitative treatments of the components of jet propulsion engines provides the tools for evaluation and component matching for optimal system performance Worked examples and end of chapter exercises provide practice for analysis, preliminary design, and systems integration

Theory of Aerospace Propulsion

Theory of Aerospace Propulsion
Author: Pasquale M Sforza
Publsiher: Butterworth-Heinemann
Total Pages: 848
Release: 2016-08-13
ISBN 10: 0128096012
ISBN 13: 9780128096017
Language: EN, FR, DE, ES & NL

Theory of Aerospace Propulsion Book Review:

Theory of Aerospace Propulsion, Second Edition, teaches engineering students how to utilize the fundamental principles of fluid mechanics and thermodynamics to analyze aircraft engines, understand the common gas turbine aircraft propulsion systems, be able to determine the applicability of each, perform system studies of aircraft engine systems for specified flight conditions and preliminary aerothermal design of turbomachinery components, and conceive, analyze, and optimize competing preliminary designs for conventional and unconventional missions. This updated edition has been fully revised, with new content, new examples and problems, and improved illustrations to better facilitate learning of key concepts. Includes broader coverage than that found in most other books, including coverage of propellers, nuclear rockets, and space propulsion to allows analysis and design of more types of propulsion systems Provides in-depth, quantitative treatments of the components of jet propulsion engines, including the tools for evaluation and component matching for optimal system performance Contains additional worked examples and progressively challenging end-of- chapter exercises that provide practice for analysis, preliminary design, and systems integration

Theory of Aerospace Propulsion

Theory of Aerospace Propulsion
Author: Pasquale M Sforza
Publsiher: Elsevier
Total Pages: 704
Release: 2011-09-27
ISBN 10: 012384889X
ISBN 13: 9780123848895
Language: EN, FR, DE, ES & NL

Theory of Aerospace Propulsion Book Review:

Theory of Aerospace Propulsion provides excellent coverage of aerospace propulsion systems, including propellers, nuclear rockets, and space propulsion. The book's in-depth, quantitative treatment of the components of jet propulsion engines provides the tools for evaluation and component matching for optimal system performance. Worked examples and end of chapter exercises provide practice for analysis, preliminary design, and systems integration. Readers of this book will be able to utilize the fundamental principles of fluid mechanics and thermodynamics to analyze aircraft engines; understand the common gas turbine aircraft propulsion systems and be able to determine the applicability of each; perform system studies of aircraft engine systems for specified flight conditions; perform preliminary aerothermal design of turbomachinery components; conceive, analyze, and optimize competing preliminary designs for conventional and unconventional missions. The book is organized into 15 chapters covering a wide array of topics such as idealized flow machines; quasi-one-dimensional flow equations; idealized cycle analysis of jet engines; combustion chambers for airbreathing engines; nozzles and inlets; turbomachinery; blade element analysis of axial flow turbomachines; turbine engine performance and component integration; propellers; liquid rockets; solid propellant rockets; nuclear rockets; space propulsion; and propulsion aspects of high-speed flight. This book will appeal to aerospace or mechanical engineers working in gas turbines, turbomachinery, aircraft propulsion and rocket propulsion, and to undergraduate and graduate level students in aerospace or mechanical engineering studying aerospace propulsion or turbomachinery. Early coverage of cycle analysis provides a systems perspective, and offers context for the chapters on turbomachinery and components Broader coverage than found in most other books - including coverage of propellers, nuclear rockets, and space propulsion - allows analysis and design of more types of propulsion systems In depth, quantitative treatments of the components of jet propulsion engines provides the tools for evaluation and component matching for optimal system performance Worked examples and end of chapter exercises provide practice for analysis, preliminary design, and systems integration

Aerospace Propulsion Systems

Aerospace Propulsion Systems
Author: Thomas A. Ward
Publsiher: John Wiley & Sons
Total Pages: 448
Release: 2010-05-17
ISBN 10: 0470824972
ISBN 13: 9780470824979
Language: EN, FR, DE, ES & NL

Aerospace Propulsion Systems Book Review:

Aerospace Propulsion Systems is a unique book focusing on each type of propulsion system commonly used in aerospace vehicles today: rockets, piston aero engines, gas turbine engines, ramjets, and scramjets. Dr. Thomas A. Ward introduces each system in detail, imparting an understanding of basic engineering principles, describing key functionality mechanisms used in past and modern designs, and provides guidelines for student design projects. With a balance of theory, fundamental performance analysis, and design, the book is specifically targeted to students or professionals who are new to the field and is arranged in an intuitive, systematic format to enhance learning. Covers all engine types, including piston aero engines Design principles presented in historical order for progressive understanding Focuses on major elements to avoid overwhelming or confusing readers Presents example systems from the US, the UK, Germany, Russia, Europe, China, Japan, and India Richly illustrated with detailed photographs Cartoon panels present the subject in an interesting, easy-to-understand way Contains carefully constructed problems (with a solution manual available to the educator) Lecture slides and additional problem sets for instructor use Advanced undergraduate students, graduate students and engineering professionals new to the area of propulsion will find Aerospace Propulsion Systems a highly accessible guide to grasping the key essentials. Field experts will also find that the book is a very useful resource for explaining propulsion issues or technology to engineers, technicians, businessmen, or policy makers. Post-graduates involved in multi-disciplinary research or anybody interested in learning more about spacecraft, aircraft, or engineering would find this book to be a helpful reference. Lecture materials for instructors available at www.wiley.com/go/wardaero

Aerospace Propulsion

Aerospace Propulsion
Author: T. W. Lee
Publsiher: John Wiley & Sons
Total Pages: 320
Release: 2013-10-18
ISBN 10: 1118534875
ISBN 13: 9781118534878
Language: EN, FR, DE, ES & NL

Aerospace Propulsion Book Review:

Aerospace propulsion devices embody some of the most advancedtechnologies, ranging from materials, fluid control, and heattransfer and combustion. In order to maximize the performance,sophisticated testing and computer simulation tools are developedand used. Aerospace Propulsion comprehensively covers the mechanicsand thermal-fluid aspects of aerospace propulsion, starting fromthe fundamental principles, and covering applications togas-turbine and space propulsion (rocket) systems. It presentsmodern analytical methods using MATLAB and other advanced softwareand includes essential elements of both gas-turbine and rocketpropulsion systems. Gas turbine coverage includes thermodynamicanalysis, turbine components, diffusers, compressors, turbines,nozzles, compressor-turbine matching, combustors and afterburners.Rocket coverage includes chemical rockets, electrical rockets,nuclear and solar sail. Key features: Both gas-turbine and rocket propulsion covered in a singlevolume Presents modern analytical methods and examples Combines fundamentals and applications, including spaceapplications Accompanied by a website containing MATLAB examples, problemsets and solutions Aerospace Propulsion is a comprehensive textbook forsenior undergraduate graduate and aerospace propulsion courses, andis also an excellent reference for researchers and practicingengineers working in this area.

Powered Flight

Powered Flight
Author: David R. Greatrix
Publsiher: Springer Science & Business Media
Total Pages: 526
Release: 2012-01-25
ISBN 10: 1447124855
ISBN 13: 9781447124856
Language: EN, FR, DE, ES & NL

Powered Flight Book Review:

Whilst most contemporary books in the aerospace propulsion field are dedicated primarily to gas turbine engines, there is often little or no coverage of other propulsion systems and devices such as propeller and helicopter rotors or detailed attention to rocket engines. By taking a wider viewpoint, Powered Flight - The Engineering of Aerospace Propulsion aims to provide a broader context, allowing observations and comparisons to be made across systems that are overlooked by focusing on a single aspect alone. The physics and history of aerospace propulsion are built on step-by-step, coupled with the development of an appreciation for the mathematics involved in the science and engineering of propulsion. Combining the author’s experience as a researcher, an industry professional and a lecturer in graduate and undergraduate aerospace engineering, Powered Flight - The Engineering of Aerospace Propulsion covers its subject matter both theoretically and with an awareness of the practicalities of the industry. To ensure that the content is clear, representative but also interesting the text is complimented by a range of relevant graphs and photographs including representative engineering, in addition to several propeller performance charts. These items provide excellent reference and support materials for graduate and undergraduate projects and exercises. Students in the field of aerospace engineering will find that Powered Flight - The Engineering of Aerospace Propulsion supports their studies from the introductory stage and throughout more intensive follow-on studies.

Aircraft Propulsion

Aircraft Propulsion
Author: Saeed Farokhi
Publsiher: John Wiley & Sons
Total Pages: 1048
Release: 2014-04-01
ISBN 10: 111880676X
ISBN 13: 9781118806760
Language: EN, FR, DE, ES & NL

Aircraft Propulsion Book Review:

New edition of the successful textbook updated to include new material on UAVs, design guidelines in aircraft engine component systems and additional end of chapter problems Aircraft Propulsion, Second Edition follows the successful first edition textbook with comprehensive treatment of the subjects in airbreathing propulsion, from the basic principles to more advanced treatments in engine components and system integration. This new edition has been extensively updated to include a number of new and important topics. A chapter is now included on General Aviation and Uninhabited Aerial Vehicle (UAV) Propulsion Systems that includes a discussion on electric and hybrid propulsion. Propeller theory is added to the presentation of turboprop engines. A new section in cycle analysis treats Ultra-High Bypass (UHB) and Geared Turbofan engines. New material on drop-in biofuels and design for sustainability is added to refl ect the FAA’s 2025 Vision. In addition, the design guidelines in aircraft engine components are expanded to make the book user friendly for engine designers. Extensive review material and derivations are included to help the reader navigate through the subject with ease. Key features: General Aviation and UAV Propulsion Systems are presented in a new chapter Discusses Ultra-High Bypass and Geared Turbofan engines Presents alternative drop-in jet fuels Expands on engine components' design guidelines The end-of-chapter problem sets have been increased by nearly 50% and solutions are available on a companion website Presents a new section on engine performance testing and instrumentation Includes a new 10-Minute Quiz appendix (with 45 quizzes) that can be used as a continuous assessment and improvement tool in teaching/learning propulsion principles and concepts Includes a new appendix on Rules of Thumb and Trends in aircraft propulsion Aircraft Propulsion, Second Edition is a must-have textbook for graduate and undergraduate students, and is also an excellent source of information for researchers and practitioners in the aerospace and power industry.

Jet Propulsion

Jet Propulsion
Author: Nicholas Cumpsty,Andrew Heyes
Publsiher: Cambridge University Press
Total Pages: 365
Release: 2015-07-22
ISBN 10: 1107511224
ISBN 13: 9781107511224
Language: EN, FR, DE, ES & NL

Jet Propulsion Book Review:

This book is an introduction to the design of modern civil and military jet engines using engine design projects.

Fundamentals of Aircraft and Rocket Propulsion

Fundamentals of Aircraft and Rocket Propulsion
Author: Ahmed F. El-Sayed
Publsiher: Springer
Total Pages: 1010
Release: 2016-05-25
ISBN 10: 1447167961
ISBN 13: 9781447167969
Language: EN, FR, DE, ES & NL

Fundamentals of Aircraft and Rocket Propulsion Book Review:

This book provides a comprehensive basics-to-advanced course in an aero-thermal science vital to the design of engines for either type of craft. The text classifies engines powering aircraft and single/multi-stage rockets, and derives performance parameters for both from basic aerodynamics and thermodynamics laws. Each type of engine is analyzed for optimum performance goals, and mission-appropriate engines selection is explained. Fundamentals of Aircraft and Rocket Propulsion provides information about and analyses of: thermodynamic cycles of shaft engines (piston, turboprop, turboshaft and propfan); jet engines (pulsejet, pulse detonation engine, ramjet, scramjet, turbojet and turbofan); chemical and non-chemical rocket engines; conceptual design of modular rocket engines (combustor, nozzle and turbopumps); and conceptual design of different modules of aero-engines in their design and off-design state. Aimed at graduate and final-year undergraduate students, this textbook provides a thorough grounding in the history and classification of both aircraft and rocket engines, important design features of all the engines detailed, and particular consideration of special aircraft such as unmanned aerial and short/vertical takeoff and landing aircraft. End-of-chapter exercises make this a valuable student resource, and the provision of a downloadable solutions manual will be of further benefit for course instructors.

Jet Rocket Nuclear Ion and Electric Propulsion

Jet  Rocket  Nuclear  Ion and Electric Propulsion
Author: W.H.T. Loh
Publsiher: Springer Science & Business Media
Total Pages: 766
Release: 2012-12-06
ISBN 10: 3642461093
ISBN 13: 9783642461095
Language: EN, FR, DE, ES & NL

Jet Rocket Nuclear Ion and Electric Propulsion Book Review:

During the last decade, rapid growth of knowledge in the field of jet, rocket, nuclear, ion and electric propulsion has resulted in many advances useful to the student, engineer and scientist. The purpose for offering this course is to make available to them these recent advances in theory and design. Accordingly, this course is organized into seven parts: Part 1 Introduction; Part 2 Jet Propulsion; Part 3 Rocket Propulsion; Part 4 Nuclear Propulsion; Part 5 Electric and Ion Propulsion; Part 6 Theory on Combustion, Detonation and Fluid Injection; Part 7 Advanced Concepts and Mission Applications. It is written in such a way that it may easily be adopted by other universities as a textbook for a one semester senior or graduate course on the subject. In addition to the undersigned who served as the course instructor and wrote Chapter I, 2 and 3, guest lecturers included: DR. G. L. DUGGER who wrote Chapter 4 "Ram-jets and Air-Aug mented Rockets," DR. GEORGE P. SUTTON who wrote Chapter 5 "Rockets and Cooling Methods," DR . . MARTIN SUMMERFIELD who wrote Chapter 6 "Solid Propellant Rockets," DR. HOWARD S. SEIFERT who wrote Chapter 7 "Hybrid Rockets," DR. CHANDLER C. Ross who wrote Chapter 8 "Advanced Nuclear Rocket Design," MR. GEORGE H. McLAFFERTY who wrote Chapter 9 "Gaseous Nuclear Rockets," DR. S. G. FORBES who wrote Chapter 10 "Electric and Ion Propul sion," DR. R. H. BODEN who wrote Chapter 11 "Ion Propulsion," DR.

Introduction to Aerospace Propulsion

Introduction to Aerospace Propulsion
Author: R. Douglas Archer,Maido Saarlas
Publsiher: Unknown
Total Pages: 582
Release: 1996
ISBN 10:
ISBN 13: UOM:39015048082856
Language: EN, FR, DE, ES & NL

Introduction to Aerospace Propulsion Book Review:

This work introduces students to the amazing and impressive expanse of propulsion systems used in aeronautics and aerospace, ranging from the piston engine and propeller to the rocket. Many examples and problems are included to illustrate the principles common to all propulsion types. Through this approach, students can develop an understanding of the reasons for trends and limitations in design and performance as well as explore the similarities between the types. Intended for use as an undergraduate text, this work should also be a useful reference for practising engineers.

Rocket Propulsion

Rocket Propulsion
Author: Stephen D. Heister,William E. Anderson,Timothée L. Pourpoint,R. Joseph Cassady
Publsiher: Cambridge University Press
Total Pages: 510
Release: 2019-02-07
ISBN 10: 1108422276
ISBN 13: 9781108422277
Language: EN, FR, DE, ES & NL

Rocket Propulsion Book Review:

Equips students with an up-to-date practical knowledge of rocket propulsion, numerous homework problems, and online self-study materials.

Aircraft Propulsion

Aircraft Propulsion
Author: Saeed Farokhi
Publsiher: John Wiley & Sons Incorporated
Total Pages: 786
Release: 2009
ISBN 10:
ISBN 13: STANFORD:36105131716644
Language: EN, FR, DE, ES & NL

Aircraft Propulsion Book Review:

"Aircrarft Propulsion presents thorough coverage of fundamental concepts along with numerous detailed examples and extensive illustrations. This accessible introduction first discusses compressible flow with heat and friction as well as engine thrust and performance parameters. Readers will then learn about aircraft gas turbine engine cycles followed by aircraft engine components. And they'll discover the aerodynamics and performance of centrifugal compressors." -- Publisher description.

Aircraft Propulsion Systems Technology and Design

Aircraft Propulsion Systems Technology and Design
Author: Gordon C. Oates
Publsiher: AIAA
Total Pages: 535
Release: 1989
ISBN 10: 9781600860218
ISBN 13: 1600860214
Language: EN, FR, DE, ES & NL

Aircraft Propulsion Systems Technology and Design Book Review:

Principles of Nuclear Rocket Propulsion

Principles of Nuclear Rocket Propulsion
Author: William J. Emrich, Jr.
Publsiher: Butterworth-Heinemann
Total Pages: 344
Release: 2016-07-28
ISBN 10: 0128045302
ISBN 13: 9780128045305
Language: EN, FR, DE, ES & NL

Principles of Nuclear Rocket Propulsion Book Review:

Principles of Nuclear Rocket Propulsion provides an understanding of the physical principles underlying the design and operation of nuclear fission-based rocket engines. While there are numerous texts available describing rocket engine theory and nuclear reactor theory, this is the first book available describing the integration of the two subject areas. Most of the book’s emphasis is primarily on nuclear thermal rocket engines, wherein the energy of a nuclear reactor is used to heat a propellant to high temperatures and then expel it through a nozzle to produce thrust. Other concepts are also touched upon such as a section devoted to the nuclear pulse rocket concept wherein the force of externally detonated nuclear explosions is used to accelerate a spacecraft. Future crewed space missions beyond low earth orbit will almost certainly require propulsion systems with performance levels exceeding that of today’s best chemical engines. A likely candidate for that propulsion system is the solid core Nuclear Thermal Rocket or NTR. Solid core NTR engines are expected to have performance levels which significantly exceed that achievable by any currently conceivable chemical engine. The challenge is in the engineering details of the design which includes not only the thermal, fluid, and mechanical aspects always present in chemical rocket engine development, but also nuclear interactions and some unique materials restrictions. Sorts and organizes information on various types of nuclear thermal rocket engines into a coherent curriculum Includes a number of example problems to illustrate the concepts being presented Features a companion site with interactive calculators demonstrating how variations in the constituent parameters affect the physical process being described Includes 3D figures that may be scaled and rotated to better visualize the nature of the object under study

Fundamentals of Jet Propulsion with Applications

Fundamentals of Jet Propulsion with Applications
Author: Ronald D. Flack
Publsiher: Cambridge University Press
Total Pages: 329
Release: 2005-04-25
ISBN 10: 1107393884
ISBN 13: 9781107393882
Language: EN, FR, DE, ES & NL

Fundamentals of Jet Propulsion with Applications Book Review:

This introductory 2005 text on air-breathing jet propulsion focuses on the basic operating principles of jet engines and gas turbines. Previous coursework in fluid mechanics and thermodynamics is elucidated and applied to help the student understand and predict the characteristics of engine components and various types of engines and power gas turbines. Numerous examples help the reader appreciate the methods and differing, representative physical parameters. A capstone chapter integrates the text material into a portion of the book devoted to system matching and analysis so that engine performance can be predicted for both on- and off-design conditions. The book is designed for advanced undergraduate and first-year graduate students in aerospace and mechanical engineering. A basic understanding of fluid dynamics and thermodynamics is presumed. Although aircraft propulsion is the focus, the material can also be used to study ground- and marine-based gas turbines and turbomachinery and some advanced topics in compressors and turbines.

Future Propulsion Systems and Energy Sources in Sustainable Aviation

Future Propulsion Systems and Energy Sources in Sustainable Aviation
Author: Saeed Farokhi
Publsiher: John Wiley & Sons
Total Pages: 448
Release: 2020-01-28
ISBN 10: 1119414997
ISBN 13: 9781119414995
Language: EN, FR, DE, ES & NL

Future Propulsion Systems and Energy Sources in Sustainable Aviation Book Review:

A comprehensive review of the science and engineering behind future propulsion systems and energy sources in sustainable aviation Future Propulsion Systems and Energy Sources: in sustainable aviation is a comprehensive reference that offers a review of the science and engineering principles that underpin the concepts of propulsion systems and energy sources in sustainable air transportation. The author – a noted expert in the field – examines the impact of air transportation on the environment and reviews alternative jet fuels, hybrid-electric and nuclear propulsion and power. He also explores modern propulsion for transonic and supersonic-hypersonic aircraft and the impact of propulsion on aircraft design. Climate change is the main driver for the new technology development in sustainable air transportation. The book contains critical review of gas turbine propulsion and aircraft aerodynamics; followed by an insightful presentation of the aviation impact on environment. Future fuels and energy sources are introduced in a separate chapter. Promising technologies in propulsion and energy sources are identified leading to pathways to sustainable aviation. To facilitate the utility of the subject, the book is accompanied by a website that contains illustrations, and equation files. This important book: Contains a comprehensive reference to the science and engineering behind propulsion and power in sustainable air transportation Examines the impact of air transportation on the environment Covers alternative jet fuels and hybrid-electric propulsion and power Discusses modern propulsion for transonic, supersonic and hypersonic aircraft Examines the impact of propulsion system integration on aircraft design Written for engineers, graduate and senior undergraduate students in mechanical and aerospace engineering, Future Propulsion Systems and Energy Sources: in sustainable aviation explores the future of aviation with a guide to sustainable air transportation that includes alternative jet fuels, hybrid-electric propulsion, all-electric and nuclear propulsion.

Commercial Aircraft Propulsion and Energy Systems Research

Commercial Aircraft Propulsion and Energy Systems Research
Author: National Academies of Sciences, Engineering, and Medicine,Division on Engineering and Physical Sciences,Aeronautics and Space Engineering Board,Committee on Propulsion and Energy Systems to Reduce Commercial Aviation Carbon Emissions
Publsiher: National Academies Press
Total Pages: 122
Release: 2016-09-09
ISBN 10: 0309440963
ISBN 13: 9780309440967
Language: EN, FR, DE, ES & NL

Commercial Aircraft Propulsion and Energy Systems Research Book Review:

The primary human activities that release carbon dioxide (CO2) into the atmosphere are the combustion of fossil fuels (coal, natural gas, and oil) to generate electricity, the provision of energy for transportation, and as a consequence of some industrial processes. Although aviation CO2 emissions only make up approximately 2.0 to 2.5 percent of total global annual CO2 emissions, research to reduce CO2 emissions is urgent because (1) such reductions may be legislated even as commercial air travel grows, (2) because it takes new technology a long time to propagate into and through the aviation fleet, and (3) because of the ongoing impact of global CO2 emissions. Commercial Aircraft Propulsion and Energy Systems Research develops a national research agenda for reducing CO2 emissions from commercial aviation. This report focuses on propulsion and energy technologies for reducing carbon emissions from large, commercial aircraftâ€" single-aisle and twin-aisle aircraft that carry 100 or more passengersâ€"because such aircraft account for more than 90 percent of global emissions from commercial aircraft. Moreover, while smaller aircraft also emit CO2, they make only a minor contribution to global emissions, and many technologies that reduce CO2 emissions for large aircraft also apply to smaller aircraft. As commercial aviation continues to grow in terms of revenue-passenger miles and cargo ton miles, CO2 emissions are expected to increase. To reduce the contribution of aviation to climate change, it is essential to improve the effectiveness of ongoing efforts to reduce emissions and initiate research into new approaches.

Commercial Airplane Design Principles

Commercial Airplane Design Principles
Author: Pasquale M Sforza
Publsiher: Elsevier
Total Pages: 622
Release: 2014-01-31
ISBN 10: 0124199771
ISBN 13: 9780124199774
Language: EN, FR, DE, ES & NL

Commercial Airplane Design Principles Book Review:

Commercial Airplane Design Principles is a succinct, focused text covering all the information required at the preliminary stage of aircraft design: initial sizing and weight estimation, fuselage design, engine selection, aerodynamic analysis, stability and control, drag estimation, performance analysis, and economic analysis. The text places emphasis on making informed choices from an array of competing options, and developing the confidence to do so. Shows the use of standard, empirical, and classical methods in support of the design process Explains the preparation of a professional quality design report Provides a sample outline of a design report Can be used in conjunction with Sforza, Commercial Aircraft Design Principles to form a complete course in Aircraft/Spacecraft Design

Secrets of Antigravity Propulsion

Secrets of Antigravity Propulsion
Author: Paul A. LaViolette
Publsiher: Simon and Schuster
Total Pages: 512
Release: 2008-07-10
ISBN 10: 1591439906
ISBN 13: 9781591439905
Language: EN, FR, DE, ES & NL

Secrets of Antigravity Propulsion Book Review:

A complete investigation of the development and suppression of antigravity and field propulsion technologies • Reveals advanced aerospace technologies capable of controlling gravity that could revolutionize air travel and energy production • Reviews numerous field propulsion devices that have thrust-to-power ratios thousands of times greater than a jet engine • Shows how NASA participates in a cover-up to block adoption of advanced technologies under military development In Secrets of Antigravity Propulsion, physicist Paul LaViolette reveals the secret history of antigravity experimentation--from Nikola Tesla and T. Townsend Brown to the B-2 Advanced Technology Bomber. He discloses the existence of advanced gravity-control technologies, under secret military development for decades, that could revolutionize air travel and energy production. Included among the secret projects he reveals is the research of Project Skyvault to develop an aerospace propulsion system using intense beams of microwave energy similar to that used by the strange crafts seen flying over Area 51. Using subquantum kinetics--the science behind antigravity technology--LaViolette reviews numerous field-propulsion devices and technologies that have thrust-to-power ratios thousands of times greater than that of a jet engine and whose effects are not explained by conventional physics and relativity theory. He then presents controversial evidence about the NASA cover-up in adopting these advanced technologies. He also details ongoing Russian research to duplicate John Searl’s self-propelled levitating disc and shows how the results of the Podkletnov gravity beam experiment could be harnessed to produce an interstellar spacecraft.