[PDF] Materials Compatibility With Liquid Rocket Propellants eBook

Author : Walter K. Boyd
Publisher :
Page : 46 pages
File Size : 31,68 MB
Release : 1965
Category : Liquid propellants
ISBN :

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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.

Author :
Publisher :
Page : 122 pages
File Size : 26,24 MB
Release : 1970
Category :
ISBN :

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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.

Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 102 pages
File Size : 48,65 MB
Release : 2018-07-18
Category :
ISBN : 9781723201622

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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...

Author : John Drury Clark
Publisher : Rutgers University Press
Page : 232 pages
File Size : 20,90 MB
Release : 1972-02-14
Category : Science
ISBN : 0813585244

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A classic, accessible, and entertaing history of liquid rocket propellants, with introduction by Isaac Asimov.

Author :
Publisher :
Page : 164 pages
File Size : 34,57 MB
Release : 1961
Category : Handbooks, manuals, etc
ISBN :

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"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.

Author : WILLIAM A. HOLLISTER
Publisher :
Page : 18 pages
File Size : 28,98 MB
Release : 1962
Category :
ISBN :

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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).