Compatibility Of Materials With Rocket Propellants And Oxidizers
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Compatibility Of Materials With Rocket Propellants And Oxidizers
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Author : Walter K. Boyd
language : en
Publisher:
Release Date : 1965
Compatibility Of Materials With Rocket Propellants And Oxidizers written by Walter K. Boyd and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Liquid propellants categories.
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.
Compatibility Of Rocket Propellants With Materials Of Construction
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Author : Walter K. Boyd
language : en
Publisher:
Release Date : 1960
Compatibility Of Rocket Propellants With Materials Of Construction written by Walter K. Boyd and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Liquid propellants categories.
Materials Compatibility With Oxidizer Rich Gases At Elevated Temperatures And Pressure
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-07-18
Materials Compatibility With Oxidizer Rich Gases At Elevated Temperatures And Pressure written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-07-18 with categories.
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...
Technical Abstract Bulletin
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Author :
language : en
Publisher:
Release Date :
Technical Abstract Bulletin written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with Science categories.
Materials Properties Handbook
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Author : Gerhard Welsch
language : en
Publisher: ASM International
Release Date : 1993-12-31
Materials Properties Handbook written by Gerhard Welsch and has been published by ASM International this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993-12-31 with Technology & Engineering categories.
Comprehensive datasheets on more than 60 titanium alloys More than 200 pages on metallurgy and fabrication procedures Input from more than 50 contributors from several countries Careful editorial review for accuracy and usefulness. Materials Properties Handbook: Titanium Alloys provides a data base for information on titanium and its alloys, and the selection of specific alloys for specific applications. The most comprehensive titanium data package ever assembled provides extensive information on applications, physical properties, corrosion, mechanical properties (including design allowances where available), fatigue, fracture properties, and elevated temperature properties. The appropriate specifications for each alloy are included. This international effort has provided a broad information base that has been compiled and reviewed by leading experts within the titanium industry, from several countries, encompassing numerous technology areas. Inputs have been obtained from the titanium industry, fabricators, users, government and academia. This up-to-date package covers information from almost the inception of the titanium industry, in the 1950s, to mid-1992. The information, organized by alloy, makes this exhaustive collection an easy-to-use data base at your fingertips, which generally includes all the product forms for each alloy. The 60-plus data sheets supply not only extensive graphical and tabular information on properties, but the datasheets also describe or illustrate important factors which would aid in the selection of the proper alloy or heat treatment. The datasheets are further supplemented with back-ground information on the metallurgy and fabrication characteristics of titanium alloys. An especially extensive coverage of properties, processing and metallurgy is provided in the datasheet for the workhorse of the titanium industry, Ti-6Al-4V. This compendium includes the newest alloys made public. even those still under development. In many cases, key references are included for further information on a given subject. Comprehensive datasheets provide extensive information on: Applications, Specifications, Corrosion, Mechanical Design Properties, Fatigue and Fracture
An Experimental Investigation Of Chemical Reaction Between Propellant Tank Material And Rocket Fuels Or Oxidizers When Impacted By Small High Velocity Projectiles
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Author : Robert P. Dengler
language : en
Publisher:
Release Date : 1963
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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Projectiles categories.
Government Wide Index To Federal Research Development Reports
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Author :
language : en
Publisher:
Release Date : 1965
Government Wide Index To Federal Research Development Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Government publications categories.
Titan Ii Storable Propellant Handbook
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Author :
language : en
Publisher:
Release Date : 1961
Titan Ii Storable Propellant Handbook written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Handbooks, manuals, etc categories.
"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.
Rocket Propellants
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Author : Francis A. Warren
language : en
Publisher:
Release Date : 1958
Rocket Propellants written by Francis A. Warren and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Rockets (Aeronautics) categories.
Fast Reactions In Energetic Materials
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Author : Alexander S. Shteinberg
language : en
Publisher: Springer Science & Business Media
Release Date : 2008-09-26
Fast Reactions In Energetic Materials written by Alexander S. Shteinberg and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 2008-09-26 with Science categories.
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.