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Hybrid combustion with metallized fuelsA chemical method of adding certain catalysts to improve the degradation process of a solid fuel is discussed. Thermogravimetric (TGA) analysis used to study the fundamental degradation behavior of a typical hybrid fuel (HTPB) shows that high surface temperatures increase the degradation rate. Fuels were tested in a laboratory-scale experimental hybrid rocket and their behavior was compared to a baseline behavior of HTPB fuel regression rates. It was found that a small amount of metal powder added to the fuel can significantly increase the regression rates.
Document ID
19930066174
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yi, Jianwen
(NASA Headquarters Washington, DC United States)
Wygle, Brian S.
(NASA Headquarters Washington, DC United States)
Bates, Ronald W.
(NASA Headquarters Washington, DC United States)
Jones, Michael D.
(NASA Headquarters Washington, DC United States)
Ramohalli, Kumar
(Arizona Univ. Tucson, United States)
Date Acquired
August 16, 2013
Publication Date
June 1, 1993
Subject Category
Propellants And Fuels
Report/Patent Number
AIAA PAPER 93-2410
Meeting Information
Meeting: AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: June 28, 1993
End Date: June 30, 1993
Sponsors: ASEE, SAE, AIAA, ASME
Accession Number
93A50171
Distribution Limits
Public
Copyright
Other

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