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Compatibility Studies of Hydrogen Peroxide and a New Hypergolic Fuel BlendSeveral preliminary materials compatibility studies have been conducted to determine the practicality of a new hypergolic fuel system. Hypergolic fuel ignites spontaneously as the oxidizer decomposes and releases energy in the presence of the fuel. The bipropellant system tested consists of high-test hydrogen peroxide (HTP) and a liquid fuel blend consisting of a hydrocarbon fuel, an ignition enhancer and a transition metal catalyst. In order for further testing of the new fuel blend to take place, some basic materials compatibility and HTP decomposition studies must be accomplished. The thermal decomposition rate of HTP was tested using gas evolution and isothermal microcalorimetry (IMC). Materials were analyzed for compatibility with hydrogen peroxide including a study of the affect welding has on stainless steel elemental composition and its relation to HTP decomposition. Compatibility studies of valve materials in the fuel blend were performed to determine the corrosion resistance of the materials.
Document ID
20030059515
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Baldridge, Jennifer
(Auburn Univ. AL, United States)
Villegas, Yvonne
(Alabama Univ. Huntsville, AL, United States)
Date Acquired
September 7, 2013
Publication Date
August 9, 2002
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: NASA-MSFC 2002 Undergraduate Student Research Program Technical Report Collection
Location: Huntsville, AL
Country: United States
Start Date: November 1, 2002
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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