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Thermodynamic And Ballistic Design Fundamentals Of Solid Propellant Rocket Engines Selected Chapters
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Book Synopsis Thermodynamic and Ballistic Design Fundamentals of Solid-Propellant Rocket Engines (Selected Chapters). by : B. V. Orlov
Download or read book Thermodynamic and Ballistic Design Fundamentals of Solid-Propellant Rocket Engines (Selected Chapters). written by B. V. Orlov and published by . This book was released on 1970 with total page 242 pages. Available in PDF, EPUB and Kindle. Book excerpt: The book gives an account of thermodynamic principles of the calculation of solid-propellant rocket engines, engineering methods of the calculation of processes of heat exchange, principles of the theory of the combustion of solid propellants and the calculation of the indicating pressure curve in the combustion chamber of an engine. Basic information is given concerning solid rocket propellants and heat-proof coverings used in solid-propellant rocket engines. Thrust control in these rocket engines with respect to magnitude and direction and also the general method of ballistic design of solid-propellant rockets are discussed. The solution of simplified problems of interior ballistics of classical artillery and recoilless weapons is covered, and a solution is given for three expressions of the law of the combustion of the solid propellant. (Author).
Book Synopsis Thermodynamic and Ballistic Principles for the Design of Solid-propellant Rocket Engines (selected Chapters). by : B. V. Orlov
Download or read book Thermodynamic and Ballistic Principles for the Design of Solid-propellant Rocket Engines (selected Chapters). written by B. V. Orlov and published by . This book was released on 1970 with total page 284 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book, on the basis of materials published in the domestic and foreign press, presents the thermogasodynamics principles of the design of engines, the engineering methods of calculating heat exchange processes, the principles of solid propellant combustion, and the calculation of the indicator curve of pressure in the engine combustion chamber. The book gives basic information on solid propellants used in solid rocket engines. Thrust regulation in solid rocket engines and the ballistic principles of solid rocket engines are examined. The book is intended for students in higher technical education institutes and for engineers-technicians specializing in solid fuel rocket engines. (Author).
Book Synopsis Thermodynamic and Ballistic Design Fundamentals of Solid-propellant Rocket Engines by : Boris Viktorovich Orlov
Download or read book Thermodynamic and Ballistic Design Fundamentals of Solid-propellant Rocket Engines written by Boris Viktorovich Orlov and published by . This book was released on 1966 with total page 422 pages. Available in PDF, EPUB and Kindle. Book excerpt: In this book, on the basis of materials published in the Soviet and foreign press, there are expounded thermo-gas-dynamic principles of designing of rocket engines, engineering methods of calculation of processes of heat exchange, principles of the theory of burning of solid fuels and calculation of the indicated pressure curve in the combustion chamber of the engine. In it there is given basic information about solid rocket propellants applied in solid-propellant rocket engines (SPRE). There is considered regulation of thrust in SPRE in magnitude and direction, and also a general method of ballistic designing of solid-fuel rockets. (Author).
Book Synopsis Thermodynamic and Ballistic Fundamentals for Designing Rocket Engines Using Solid Propellants (Chapter V). by : B. V. Orlov
Download or read book Thermodynamic and Ballistic Fundamentals for Designing Rocket Engines Using Solid Propellants (Chapter V). written by B. V. Orlov and published by . This book was released on 1971 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt: Ordinarily the problem of the interior ballistics of solidpropellant rocket engines (SPRE) is solved in conformity with the monomial power law of fuel combustion. The suggested method permits one to find the process of change in pressure for any law of combustion of a ballistite or mixture fuel. Whtn the SPRE reaches monomial mode there can be observed three clearly defined periods of functioning of the engine: autonomous combustion of the igniter; joint combustion of the igniter and fuel; and stabilization of pressure in the SPRE chamber. (Author).
Book Synopsis Solid Rocket Propulsion Technology by : A. Davenas
Download or read book Solid Rocket Propulsion Technology written by A. Davenas and published by Newnes. This book was released on 2012-12-02 with total page 623 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book, a translation of the French title Technologie des Propergols Solides, offers otherwise unavailable information on the subject of solid propellants and their use in rocket propulsion. The fundamentals of rocket propulsion are developed in chapter one and detailed descriptions of concepts are covered in the following chapters. Specific design methods and the theoretical physics underlying them are presented, and finally the industrial production of the propellant itself is explained. The material used in the book has been collected from different countries, as the development of this field has occurred separately due to the classified nature of the subject. Thus the reader not only has an overall picture of solid rocket propulsion technology but a comprehensive view of its different developmental permutations worldwide.
Book Synopsis Chemical Rockets by : Subramaniam Krishnan
Download or read book Chemical Rockets written by Subramaniam Krishnan and published by Springer Nature. This book was released on 2019-10-10 with total page 538 pages. Available in PDF, EPUB and Kindle. Book excerpt: The purpose of this book is to discuss, at the graduate level, the methods of performance prediction for chemical rocket propulsion. A pedagogical presentation of such methods has been unavailable thus far and this text, based upon lectures, fills this gap. The first part contains the energy-minimization to calculate the propellant-combustion composition and the subsequent computation of rocket performance. While incremental analysis is for high performance solid motors, equilibrium-pressure analysis is for low performance ones. Both are detailed in the book's second part for the prediction of ignition and tail-off transients, and equilibrium operation. Computer codes, adopting the incremental analysis along with erosive burning effect, are included. The material is encouraged to be used and presented at lectures. Senior undergraduate and graduate students in universities, as well as practicing engineers and scientists in rocket industries, form the readership.
Book Synopsis Rocket Propulsion Elements by : George P. Sutton
Download or read book Rocket Propulsion Elements written by George P. Sutton and published by John Wiley & Sons. This book was released on 2011-09-09 with total page 657 pages. Available in PDF, EPUB and Kindle. Book excerpt: The definitive text on rocket propulsion—now revised to reflect advancements in the field For sixty years, Sutton's Rocket Propulsion Elements has been regarded as the single most authoritative sourcebook on rocket propulsion technology. As with the previous edition, coauthored with Oscar Biblarz, the Eighth Edition of Rocket Propulsion Elements offers a thorough introduction to basic principles of rocket propulsion for guided missiles, space flight, or satellite flight. It describes the physical mechanisms and designs for various types of rockets' and provides an understanding of how rocket propulsion is applied to flying vehicles. Updated and strengthened throughout, the Eighth Edition explores: The fundamentals of rocket propulsion, its essential technologies, and its key design rationale The various types of rocket propulsion systems, physical phenomena, and essential relationships The latest advances in the field such as changes in materials, systems design, propellants, applications, and manufacturing technologies, with a separate new chapter devoted to turbopumps Liquid propellant rocket engines and solid propellant rocket motors, the two most prevalent of the rocket propulsion systems, with in-depth consideration of advances in hybrid rockets and electrical space propulsion Comprehensive and coherently organized, this seminal text guides readers evenhandedly through the complex factors that shape rocket propulsion, with both theory and practical design considerations. Professional engineers in the aerospace and defense industries as well as students in mechanical and aerospace engineering will find this updated classic indispensable for its scope of coverage and utility.
Book Synopsis Rocket Propulsion Elements by : George Paul Sutton
Download or read book Rocket Propulsion Elements written by George Paul Sutton and published by Wiley-Interscience. This book was released on 1986 with total page 392 pages. Available in PDF, EPUB and Kindle. Book excerpt: A revision of the standard text on the basic technology, performance and design rationale of rocket propulsion. After discussing fundamentals, such as nozzle thermodynamics, heat transfer, flight performance and chemical reaction analysis, the book continues with treatments of various types of liquid and solid propellants and rocket testing. It brings together the engineering science disciplines necessary for rocket design: thermodynamics, heat transfer, flight mechanics, chemical reactions and materials behavior. SI units and information on computer-aided testing have also been added.
Book Synopsis Fundamentals of Rocket Propulsion by : DP Mishra
Download or read book Fundamentals of Rocket Propulsion written by DP Mishra and published by CRC Press. This book was released on 2017-07-20 with total page 364 pages. Available in PDF, EPUB and Kindle. Book excerpt: The book follows a unified approach to present the basic principles of rocket propulsion in concise and lucid form. This textbook comprises of ten chapters ranging from brief introduction and elements of rocket propulsion, aerothermodynamics to solid, liquid and hybrid propellant rocket engines with chapter on electrical propulsion. Worked out examples are also provided at the end of chapter for understanding uncertainty analysis. This book is designed and developed as an introductory text on the fundamental aspects of rocket propulsion for both undergraduate and graduate students. It is also aimed towards practicing engineers in the field of space engineering. This comprehensive guide also provides adequate problems for audience to understand intricate aspects of rocket propulsion enabling them to design and develop rocket engines for peaceful purposes.
Book Synopsis Research and Development of Materiel, Engineering Design Handbook, Ballistic Missile Series, Propulsion and Propellants by :
Download or read book Research and Development of Materiel, Engineering Design Handbook, Ballistic Missile Series, Propulsion and Propellants written by and published by . This book was released on 1963 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Fundamentals of Aircraft and Rocket Propulsion by : Ahmed F. El-Sayed
Download or read book Fundamentals of Aircraft and Rocket Propulsion written by Ahmed F. El-Sayed and published by Springer. This book was released on 2016-06-06 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Solid Propellant Processing Factors in Rocket Motor Design by : Carlton L. Horine
Download or read book Solid Propellant Processing Factors in Rocket Motor Design written by Carlton L. Horine and published by . This book was released on 1971 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Solid Rocket Motor Performance Analysis and Prediction by : William H. Miller
Download or read book Solid Rocket Motor Performance Analysis and Prediction written by William H. Miller and published by . This book was released on 1971 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 812 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Thermofluiddynamics of Optimized Rocket Propulsions by : STRAUB
Download or read book Thermofluiddynamics of Optimized Rocket Propulsions written by STRAUB and published by Birkhäuser. This book was released on 2012-12-06 with total page 267 pages. Available in PDF, EPUB and Kindle. Book excerpt: This study has two declared aims: it presents the theoretical basis for a provably ideal comparative process for relaxing flows (ICP) and jus tifies its application to jet and, in particular, rocket engines. This will be treated in two parts. Part I offers a status quo report on current calculation methods, and compiles and explains briefly the most important data on selected pro minent rocket engines. Starting from the phenomenology of the dynamical and physico-chemical conversion processes in the fuel-oxidizer fluid mixture and in the burned gases, the ideal thermodynamic comparative process is then derived - as a defined sequential change of states in the system. In order to render this comparative process readily under standable, it is first applied to an appropriate model gas using alge braic equations for all relevant parameters. This model gas undergoes energy conversion processes without forfeiting the simplicity of pre sentation typical of classical gas dynamics. Above all, examination of this model offers proof that it is generally impermissible to use, as is done in practice, the familiar isentropic equation for flow changes of state continuously propagated in flow tube theory. Elementary calculations immediately indicate essential attributes which are also typical for relaxing, multicomponent, one-phase systems, such as the significant 'pressure drop phenomenon' or the establishment of the steady mass flow rate as an 'eigenvalue' of the comparative pro cess. Their relevance to the RE theory is stressed.
Book Synopsis Fundamentals of Solid-propellant Combustion by : Kenneth K. Kuo
Download or read book Fundamentals of Solid-propellant Combustion written by Kenneth K. Kuo and published by . This book was released on 1984 with total page 922 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Bibliography of Scientific and Industrial Reports by :
Download or read book Bibliography of Scientific and Industrial Reports written by and published by . This book was released on 1970 with total page 922 pages. Available in PDF, EPUB and Kindle. Book excerpt:
