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 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 Materials Compatibility with Oxidizer Rich Gases at Elevated Temperatures and Pressure written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-18 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of oxygen compatibility and resistance to ignition of candidate materials for use in a liquid rocket engine designed to incorporate an oxidizer rich preburner-LOX turbopump configuration was discussed. The program was divided into two basic tasks. The first task was to develop a preliminary design of an oxidizer turbopump preburner section complete with thermal and MS Parameter analyses and to develop a conceptual design of the main injector with a preliminary engine specification as the final product. The second task was directed totally at testing materials in oxygen-rich environments. Unspecified Center HIGH ENERGY OXIDIZERS; LIQUID ROCKET PROPELLANTS; PROPELLANT PROPERTIES; ROCKET OXIDIZERS; TURBINE PUMPS; COMPATIBILITY; MATERIALS TESTS; PERFORMANCE PREDICTION; ROCKET TEST FACILITIES...
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 High Energy Propellants written by and published by . This book was released on 1964 with total page 86 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 An Experimental Investigation of Chemical Reaction Between Propellant Tank Material and Rocket Fuels Or Oxidizers when Impacted by Small High velocity Projectiles written by Robert P. Dengler and published by . This book was released on 1963 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 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 USAF Propellant Handbooks Nitric Acid Nitrogen Tetroxide Oxidizers written by and published by . This book was released on 1977 with total page 207 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Nitric Acid/Nitrogen Tetroxide Oxidizer Handbook is a compilation of engineering information on the physical and chemical properties, storage and handling, production, transportation, safety, and material compatibility of the nitric acid/nitrogen tetroxide family of oxidizers and their blends. It contains information on the following propellants: Nitric Acid (IRFNA), High Density Acid, Nitrogen Tetroxide, MON-1, MON-3, MON-10, MON-25, Minuteman Grade N2O4. The propellant handbook is intended to be used for R and D personnel and test engineers who are directly involved in the utilization of liquid rocket propellants and the design of liquid rocket propulsion systems and facilities. (Author).
Download or read book NASA Technical Note written by and published by . This book was released on 1974 with total page 926 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Solid Propellant Chemistry Combustion and Motor Interior Ballistics 1999 written by Vigor Yang and published by AIAA. This book was released on 2000 with total page 1038 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Fast Reactions in Energetic Materials written by Alexander S. Shteinberg and published by Springer Science & Business Media. This book was released on 2008-09-26 with total page 203 pages. Available in PDF, EPUB and Kindle. Book excerpt: Modern energetic materials include explosives, blasting powders, pyrotechnic m- tures and rocket propellants [1, 2]. The study of high-temperature decomposition of condensed phases of propellants and their components (liquid, solid and hybrid) is currently of special importance for the development of space-system engineering [3, 4]. To better understand the burning mechanisms (stationary, nonstationary, - steady) of composite solid propellants and their components, information about the macrokinetics of their high-temperature decomposition is required [5]. To be able to evaluate the ignition parameters and conditions of safe handling of heat-affected explosives, one needs to know the kinetic constants of their high-temperature - composition. The development of new composite solid propellants characterized by high performance characteristics (high burning rates, high thermal stability, stability to intrachamber perturbations, and other aspects) is not possible without quanti- tive data on the high-temperature decomposition of composite solid propellants and their components [6]. The same reasons have resulted in signi?cant theoretical and practical interest in the high-temperature decomposition of components of hybrid propellants. It is known that hybrid propellants have not been used very widely due to the low bu- ing (pyrolysis) rates of the polymer blocks in the combustion chambers of hybrid rocket engines. To increase the burning rates it is necessary to obtain information about their relationships to the corresponding kinetic and thermophysical prop- ties of the fuels.
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 908 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 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:
