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Solid Rocket Motor Nozzles
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Book Synopsis Solid Rocket Motor Nozzles by : United States. National Aeronautics and Space Administration
Download or read book Solid Rocket Motor Nozzles written by United States. National Aeronautics and Space Administration and published by . This book was released on 1976 with total page 152 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Fluidic Nozzle Throats in Solid Rocket Motors by : Kan Xie
Download or read book Fluidic Nozzle Throats in Solid Rocket Motors written by Kan Xie and published by Springer. This book was released on 2019-04-26 with total page 237 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book focuses on the performance and application of fluidic nozzle throats for solid rocket motors, discussing their flow details and characterization performance, as well as the influence of the particle phase on their performance. It comprehensively covers a range of fluidic nozzle throats in solid rocket motors and is richly illustrated with impressive figures and full-color photographs. It is a valuable resource for students and researchers in the fields of aeronautics, astronautics and related industries wishing to understand the fundamentals and theories of fluidic nozzle throats and engage in fluidic nozzle throat analysis and design.
Book Synopsis Solid Rocket Motor Nozzles by : United States. National Aeronautics and Space Administration
Download or read book Solid Rocket Motor Nozzles written by United States. National Aeronautics and Space Administration and published by . This book was released on 1975 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 The Optimum Design of Solid Rocket Motor Nozzles by : Fang Guoyao
Download or read book The Optimum Design of Solid Rocket Motor Nozzles written by Fang Guoyao and published by . This book was released on 1994 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Rocket-nozzle Testing and Evaluation by : E. W. Ungar
Download or read book Rocket-nozzle Testing and Evaluation written by E. W. Ungar and published by . This book was released on 1960 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Evaluation of Solid Propellant Rocket Motor Nozzles and Cases by : S. P. Gualillo
Download or read book Evaluation of Solid Propellant Rocket Motor Nozzles and Cases written by S. P. Gualillo and published by . This book was released on 1966 with total page 119 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Analysis of Solid Rocket Motor Nozzle by : P. Lapp
Download or read book Analysis of Solid Rocket Motor Nozzle written by P. Lapp and published by . This book was released on 1992 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis AN INVESTIGATION AND FEASIBILITY DEMONSTRATION OF NOZZLES FOR RESTARTABLE SOLID ROCKET MOTORS. by :
Download or read book AN INVESTIGATION AND FEASIBILITY DEMONSTRATION OF NOZZLES FOR RESTARTABLE SOLID ROCKET MOTORS. written by and published by . This book was released on 1966 with total page 417 pages. Available in PDF, EPUB and Kindle. Book excerpt: Analytical and empirical studies were conducted to define and investigate problems associated with restartable solid propellant rocket nozzles. Thermal analysis covered the complete temperature history from startup through cooldown of the duty cycle. In addition to conventional convection, conduction, and radiation, the effects of the pyrolysis gases of charring ablators were included. The structural analysis included the investigation of the thermo-elastic behavior of cylindrical and washer inserts, the existence of plastic zones, the effects of contact pressures in stacked washer inserts, and the effects of property degradation of tungsten due to grain growth. The materials investigation included tungsten-carbon reactions, tungsten grain growth and the resulting effects on properties, and the high temperature c- direction compressive deformation of pyrolytic graphite. Rocket nozzle firings were used for verification of analyses and further problem definition. It was found that the strength of tungsten is degraded by 50% or more with very slight grain growth. Large permanent c-direction compressive deformations are attainable in pyrolytic graphite above 2600 C with stresses of 7000 psi in 30 sec. Ablation of char-forming insulators provides the principal mode of cooldown by the pyrolysis process and by heat transfer to the resulting gases as they leave the nozzle. Radiation was found to be an order of magnitude lower in significance.
Book Synopsis Internal Environment of Solid Rocket Nozzles by : F. C. Price
Download or read book Internal Environment of Solid Rocket Nozzles written by F. C. Price and published by . This book was released on 1963 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study was conducted of solid propellant rocket motor nozzle environment to implement nozzle design methods. Cold flow studies with models plus hot firing tests for particle impingement and particle cloud radiation are to be used to characterize heat flux rates throughout the nozzle. This report describes the hardware buildup and schedule of heat flux tests on a molybdenum nozzle with hydrogen, oxygen, water, and varying amounts of alumina. Cold flow technique development has shown interesting particle impingement effects as a function of modeling system design and nozzle shape. The implied full scale particle impingement rates are listed for the first two cases studied. A complete report is given on a program studying radiation of a hydrogen-oxygen-alumina plume from a one-inch diameter throatless engine. High emissivity values are indicated for all but the smallest engines. (Author).
Book Synopsis Solid Rocket Motor Nozzle Flex-seal Design Sensitivity by : James R. Donat
Download or read book Solid Rocket Motor Nozzle Flex-seal Design Sensitivity written by James R. Donat and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Design and Analysis of Solid Rocket Motor Nozzle by : A. Truchot
Download or read book Design and Analysis of Solid Rocket Motor Nozzle written by A. Truchot and published by . This book was released on 1988 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: The objective of this paper is to present the different methods used to design and analyse solid rocket motor nozzles. In a preliminary phase, the typical requirements and parameters required to design a nozzle are discussed. Afterwards the general process of th design is detailed: nozzle configuration, aerodynamic contour design, selection and sizing of liners and insulators, etc. In a second step, the different systems used to control the motor thrust or to improve the performance, such as extendible exit cone, are presented. To conclude the presentation, the different steps of the nozzle analysis are presented. For each step (aerodynamic, thermal and structural) the different computer programs used are presented (principle, possibilities, limitations).
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:
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 Amateur Rocket Motor Construction by : David Sleeter
Download or read book Amateur Rocket Motor Construction written by David Sleeter and published by . This book was released on 2004 with total page 514 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Packageable High Expansion Ratio Nozzles for Solid Propellant Rocket Motor by : Robert E. Morris
Download or read book Packageable High Expansion Ratio Nozzles for Solid Propellant Rocket Motor written by Robert E. Morris and published by . This book was released on 1967 with total page 196 pages. Available in PDF, EPUB and Kindle. Book excerpt: The purpose of this program is to develop and demonstrate practical, usable, packageable exit cones which can be stored for extended periods, be deployed reliably, and be easily scaled for direct application to future high-performance solid rocket systems which include thrust vector control. This program is to be accomplished by the completion of the following four major tasks: (1) Skybolt exit cone packaging and deployment bench tests, (2) design analysis and supporting laboratory tests, (3) subscale (Genie) tests, and (4) demonstration (Skybolt) tests. This report covers the work done on Task I and Task II. Under these tasks an elastomeric Airmat exit cone was designed, fabricated and bench tested, establishing the validity of the deployment, deflection and vibration analyses. A columbium C-103 metallic exit cone designed to translate and expand under propellant gas pressure was fabricated. The bench testing was not completed in time for this report. A mechanically supported elastomeric exit cone was designed and fabricated but was not bench tested in time for this report.
Book Synopsis Captive-fired Testing of Solid Rocket Motors by : James W. Kordig
Download or read book Captive-fired Testing of Solid Rocket Motors written by James W. Kordig and published by . This book was released on 1971 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt: