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Author : Tommy M. Tsai
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Application of Plasma Spray Process in Liquid Propellant Rocket Engine Seal Tips written by Tommy M. Tsai and published by . This book was released on 1999 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : T. N. McKechnie
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Vacuum Plasma Spray Applications on Liquid Fuel Rocket Engines written by T. N. McKechnie and published by . This book was released on 1992 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 558 pages
Book Rating : 4.0/5 ( download)
Download or read book 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit written by and published by . This book was released on 1999 with total page 558 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : DP Mishra
Publisher : CRC Press
ISBN 13 : 1351708414
Total Pages : 364 pages
Book Rating : 4.3/5 (517 download)
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.
Author :
Publisher :
ISBN 13 :
Total Pages : 1032 pages
Book Rating : 4.F/5 ( download)
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1999 with total page 1032 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : R. E. Burcham
Publisher :
ISBN 13 :
Total Pages : 174 pages
Book Rating : 4.0/5 ( download)
Download or read book Liquid Rocket Engine Turbopump Rotating-shaft Seals written by R. E. Burcham and published by . This book was released on 1978 with total page 174 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 702 pages
Book Rating : 4.F/5 ( download)
Download or read book Aerospace America written by and published by . This book was released on 1999 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 371 pages
Book Rating : 4.:/5 (227 download)
Download or read book Propellant Spray Combustion Processes During Stable and Unstable Liquid Rocket Combustion written by and published by . This book was released on 1970 with total page 371 pages. Available in PDF, EPUB and Kindle. Book excerpt: The purpose of this program is the acquisition of detailed analytical and experimental information concerning the mechanisms of energy addition from propellant spray combustion to steady flow fields and propagating pressure disturbances. Data are to be obtained and used to evaluate present or formulate new expressions describing the dynamics that contribute to the coupling processes between the spray and gas flow fields. These expressions appear in steady-state and transient propellant combustion models and bear directly on the prediction of performance and onset of high frequency combustion instability in liquid propellant rocket engines. To overcome past difficulties in comparing analytical and experimental results, an experimental apparatus which produces a monodisperse propellant spray uniformly distributed throughout the combustor has been built. The motor, to be operated as a rocket engine combustor under either stable or transient conditions, provides for optical observation and is extensively instrumented to record pressure wave amplification or decay as a function of parameter variation. Test data (drop diameters, velocity and pressure wave growth or decay as functions of chamber length and initial conditions) can be input to the newly-developed combustion models and the validity of the coupling term expressions evaluated by directly comparing the resulting predictions to experimental data. These newly-developed combustion models are described in detail.
Author : Dieter K. Huzel
Publisher : AIAA
ISBN 13 : 9781600864001
Total Pages : 452 pages
Book Rating : 4.8/5 (64 download)
Download or read book Modern Engineering for Design of Liquid-Propellant Rocket Engines written by Dieter K. Huzel and published by AIAA. This book was released on 1992 with total page 452 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Program
Publisher :
ISBN 13 :
Total Pages : 576 pages
Book Rating : 4.F/5 ( download)
Download or read book NASA Patent Abstracts Bibliography written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Program and published by . This book was released on 1991 with total page 576 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 704 pages
Book Rating : 4.:/5 (31 download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : J. D. Lewis
Publisher :
ISBN 13 :
Total Pages : 29 pages
Book Rating : 4.:/5 (862 download)
Download or read book Studies of atomization and injection processes in the liquid propellant rocket engine written by J. D. Lewis and published by . This book was released on 1962 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Shamim A. Rahman
Publisher :
ISBN 13 :
Total Pages : 160 pages
Book Rating : 4.:/5 (52 download)
Download or read book Primary Atomization Study of a Swirl Coaxial Liquid Propellant Rocket Injector written by Shamim A. Rahman and published by . This book was released on 1997 with total page 160 pages. Available in PDF, EPUB and Kindle. Book excerpt: Addresses swirl-induced injection and atomization phenomena for rocket combustion applications. Swirl injectors are among the preferred means for atomizing liquid propellant in current US and Russian designed rocket engines. An experimental approach is taken which focuses primarily on the fluid injection process using non-combusting water sprays, and then applies the knowledge to measure and describe liquid oxygen spray atomization in a research rocket chamber.
Author : I. E. Smith
Publisher :
ISBN 13 :
Total Pages : 23 pages
Book Rating : 4.:/5 (227 download)
Download or read book Combustion Processes in Liquid Propellant Rocket Motors written by I. E. Smith and published by . This book was released on 1956 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : I. I. Gorev
Publisher :
ISBN 13 :
Total Pages : 416 pages
Book Rating : 4.:/5 (227 download)
Download or read book Principles of the Production of Liquid-propellant Rocket Engines written by I. I. Gorev and published by . This book was released on 1970 with total page 416 pages. Available in PDF, EPUB and Kindle. Book excerpt: The book examines the technological processes of the manufacture of the most characteristic parts, subassemblies and units of liquid-propellant rocket engines. These include the combustion chamber, turbopump unit, power frames, valves, pipelines and also the technology of unit and general assembly. Contemporary methods of the obtaining of accurate thin-walled large parts, the technology of their machining and the adaptation for the fastening of parts having little rigidity are discussed. Methods are examined for connecting thin-walled large parts by welding and brazing with the use of high-temperature solders as well as the design of special devices for welding and soldering in inert gases and a vacuum. Characteristic defects of welding and soldering and methods of detecting them are given. The technology of the manufacture of injectors, injector heads and the assembly of combustion chambers are examined. Methods of the manufacture of thin-walled pipelines of complex configuration from sheet metal, the technology of the fitting nipples, formation of corrugations, and methods of the assembly of pipelines are discussed. Methods of static and dynamic balancing of parts and subassemblies of the turbopump unit are examined. (Author).
Author : Andrei Vladimirovich Bolgarskiy
Publisher :
ISBN 13 :
Total Pages : 122 pages
Book Rating : 4.:/5 (227 download)
Download or read book Calculation of Processes in the Combustion Chamber and Nozzle of a Liquid-propellant Rocket Engine written by Andrei Vladimirovich Bolgarskiy and published by . This book was released on 1959 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt: The book is devoted to questions of combustion and discharge at high temperatures in a liquid-propellant rocket engine. It gives the detailed technique for the thermodynamic calculation of the working process, illustrated by the solution of a series of practical problems. The book offers the bases for the possibility of applying a graphical method for calculating the parameters of the liquid-propellant rocket engine, which greatly facilitates this calculation. It gives a detailed exposition of the technique of constructing such nomograms. Two nomograms for two types of propellant, constructed by the author, are appended at the end of the book. (Author).
Author : Melvin Gerstein
Publisher :
ISBN 13 :
Total Pages : 179 pages
Book Rating : 4.:/5 (227 download)
Download or read book Propellant Sprays in Liquid Rocket Engines written by Melvin Gerstein and published by . This book was released on 1966 with total page 179 pages. Available in PDF, EPUB and Kindle. Book excerpt: The research described in this report is directed at obtaining an understanding of the behavior of propellant sprays in a liquid propellant rocket engine under oscillating flow conditions as a means of relating combustion stability to propellant properties and injector design. The report covers: (1) an outline of the work on the instability problem; (2) the combustion instability model; (3) calculation of fluctuations in the vaporization of liquid sprays for axisymmetric injection; (4) preliminary formulation of a transient problem associated with pressure oscillations in a rocket chamber; (5) calculation of Green's function for the transient instability problem; (6) a simple example of the calculation of the spray distribution function and the stability criterion; and (7) perturbation method for calculating stability boundaries. Sections 2 and 3 are related to treating a linear type instability where all oscillations are acoustic in nature. Sec 4 deals with the development of finite amplitude waves. In Sec. 5 a method of solution of the transient instability problem is discussed. Sections 6 and 7 cover a sample calculation of the spray distribution function and stability criterion. Significant results show that droplet vaporization can be a cause of combustion instability and that stability boundaries can be predicted from injector parameters and propellant properties. (Author).
