Investigation of Non-Conventional Bio-Derived Fuels for Hybrid Rocket Motors
Non-conventional bio-derived fuels have been evaluated for use in hybrid rocket motors. Tests were conducted at combustion pressures in the range of 100 – 220 psig and thrust levels of 40 – 170 newtons. Beeswax was tested with oxygen as the oxidizer and showed a regression rate at least three times...
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Trace: Tennessee Research and Creative Exchange
2007
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| Online Access: | http://trace.tennessee.edu/utk_graddiss/269 |