Download or read book Compatibility of Rocket Propellants with Materials of Construction written by Walter K. Boyd and published by . This book was released on 1960 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Compatibility of Materials with Rocket Propellants and Oxidizers written by Walter K. Boyd and published by . This book was released on 1965 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: The memorandum summarizes the available information on the compatibility of liquid rocket propellants with prominent materials of construction. Fuels and oxidizers of current interest are discussed. The corrosion data which are presented will apply to storing, handling, and control equipment outside of missiles and to missile components excluding combustion chamber. The compatibility of materials with reaction products in combustion chambers, nozzles, etc., is not considered. Included in the summary are data for many nonmetallic materials. The memorandum is subdivided into sections according to the propellant. Each material of construction is rated for a given medium as belonging to one of four classes, based primarily upon corrosion resistance. Consideration also is given to such factors as catalytic decomposition and sensitivity to impact.
Download or read book The Compatiblity of Advanced Packageable Rocket Propellants with Materials of Construction written by and published by . This book was released on 1963 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt: The object of this investigation was to determine materials of construction compatible with the rocket propellants and Hydrazoid P for extended periods of time. As Army requirements demand storability at any temperature between -65 F and + 160 F, compatibility studies should emphasize the behavior of the materials investigated at the latter temperature. The two studies reported emphasize the behavior of the propellants and the construction materials at the high temperature end of the storage range. Al alloys, Ta, Ti, polyethylene, and Teflon were unaffected by Hydrazoid P. Inconel, Ni and the stainless steels were appreciably corroded and the propellant was contaminated by corrosion products. The Kel-F swelled and blistered. None of the materials tested were appreciably corroded by Cl F3. Al and Ti are recommended for tank materials for Hydrazoid P, and polyethylene and Teflon for O-ring material. Both Al and stainless steel can be recommended as tank materials for Cl F3. Teflon is the only non-metallic O-ring material recommended.
Download or read book Materials Compatibility with Liquid Rocket Propellants written by and published by . This book was released on 1970 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt: This document presents hazard documentation in the area of materials compatibility with liquid rocket propellants. The information contained herein has been collected and extracted in part from handbooks, specifications, technical reports, books, journal articles and manuals, to aid the Safety Engineer in the survey of such hazard data.
Download or read book A Rare Robert Morris Caricature written by Robert William Glenroie Vail and published by . This book was released on 1936 with total page 3 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Evolution of Rocket Engine Propellant written by G. A. Beane and published by . This book was released on 1963 with total page 11 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Titan II Storable Propellant Handbook written by and published by . This book was released on 1961 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt: "Summarized are the physical properties, materials compatibility, handling techniques, flammability and explosivity, and procedures for storing, cleaning, and flushing the Titan II propellants N2O4 as the oxidizer and a nominal 50/50 blend of UDMH and N2H4 as the fuel. The data presented was derived both from a literature survey and from a test program conducted at Bell Aerosystems Company and at the U.S. Bureau of Mines". -- page iii.
Download or read book Rocket Propellant Technology written by Jawaharlal "Ram" Ramnarace and published by Page Publishing Inc. This book was released on 2016-01-11 with total page 297 pages. Available in PDF, EPUB and Kindle. Book excerpt: Rocket Propulsion has come of age. Although its potentialities and capabilities in many areas have been recognized for centuries, it is only in recent years that scientists have had the materials and the manufacturing techniques at their command so they could control and direct the tremendous forces available. Space exploration and manned flights by astronauts have brought the science of rocketry to the attention of the general public. It has also stimulated the interest of students at all levels of advancement in the technical details of space flight. Rocket Propellant Technologies is written for serious students of astronautics. This volume reviews briefly the history of rocketry and the fundamental principles connected with rocket propulsion. Types of propellants, the chemical reactions involved, and the techniques used in manufacturing are explained. The merits of solid and liquid fuels are enumerated. Exotic propellants of the future are discussed, with reasons why their development is essential. Finally, the safety aspects of manufacturing and testing rocket propellants are given in detail. The Amateur Rocket Association under whose guidance this series has been prepared, serves as a focal point for many related activities, bringing new ideas to the attention of its members and offering suggestions for future lines of research.
Download or read book Rocket Propellants written by Defense Documentation Center (U.S.) and published by . This book was released on 1960 with total page 176 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Chemistry and Technology of Solid Rocket Propellants A Treatise on Solid Propellants written by T.L. Varghese and published by Allied Publishers. This book was released on 2017-03-29 with total page 326 pages. Available in PDF, EPUB and Kindle. Book excerpt: The book is a treatise on solid propellants in nine chapters, covering the history, chemistry, energetics, processing and characterization aspects of composite solid propellants, internal ballistics, advanced solid propellants, safety, quality and reliability and homogenous or double base propellants. The book also traces the evolution of solid propellant technology in ISRO for launch vehicles and sounding rockets. There is a detailed table of contents, expanded index, glossary, exhaustive references and questions in each chapter. It can be used as a textbook for science and engineering students, as a reference book for researchers and as a companion to scientists and engineers working in the research, development and production areas of solid propellants.
Download or read book Propellant Material Compatibility Study written by and published by . This book was released on 1971 with total page 61 pages. Available in PDF, EPUB and Kindle. Book excerpt: The objective of this program was to define the threshold sensitivity limit of hydrazine fuels in common metallic materials of construction as a function of temperature and pressure. Four propellants were included in the program: hydrazine, monomethylhydrazine, MHF-5, and MHF-7. Eleven metallic materials of construction were included in the program: stainless steel 304L, 316, 321, 347, and 17-7PH; aluminum 1100-0, 6061-T6, and 2014-T6; Inconel-X 750; Haynes-25; and Hastelloy-X. Three standard tests were used to determine the threshold sensitivity limit of the propellants in the various materials: thermal stability test, detonation propagation test, and U-tube adiabatic compression test.
Download or read book U S Government Research Reports written by and published by . This book was released on 1964 with total page 1416 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Stability and Compatibility Studies on Advanced Rocket Propellant Components written by Ivan C. Smith and published by . This book was released on 1970 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt: A number of candidate advanced propellant ingredients were studied with the objective of obtaining definitive information regarding their usefulness in new propellant systems. The research was laboratory based, involved small quantities (generally less than 100 mg.) of the ingredient, and dealt generally with the stability of individual ingredients and with stability- compatibility of two or more components of proposed propellants. The ingredients studied include: Perchlorates--HAP, HP-2, DOAP and AP (for comparison); N-F materials--P-BEP, TVOPA and P-722; Fuel--AlH3; and numerous state-of-the-art binder prepolymers and curatives.
Download or read book Material Compatibility with Space Storable Propellants Design Guidebook written by and published by . This book was released on 1972 with total page 152 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Solid Rocket Propellants written by Haridwar Singh and published by Royal Society of Chemistry. This book was released on 2019-03-07 with total page 183 pages. Available in PDF, EPUB and Kindle. Book excerpt: Propellants contain considerable chemical energy that can be used in rocket propulsion. Bringing together information on both the theoretical and practical aspects of solid rocket propellants for the first time, this book will find a unique place on the readers' shelf providing the overall picture of solid rocket propulsion technology. Aimed at students, engineers and researchers in the area, the authors have applied their wealth of knowledge regarding formulation, processing and evaluation to provide an up to date and clear text on the subject.
Download or read book Compatibility of Elastomers with Liquid Propellants an Annotated Bibliography written by WILLIAM A. HOLLISTER and published by . This book was released on 1962 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt: Fifty-two references are presented on the effects of liquid rocket propellants on elastomeric materials. The propellants investigated include inhibited red fuming nitric acid, nitrogen tetraoxide oxide, nitrogen oxide, unsymmetrical dimethylhydrazine, and hydrazine. (Author).
Download or read book WADC Technical Report written by United States. Wright Air Development Division and published by . This book was released on 1961 with total page 1246 pages. Available in PDF, EPUB and Kindle. Book excerpt:
