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Tor Viscor, Landon Kamps, Kazuo Yonekura, Hikaru Isochi and Harunori Nagata
An understanding of the scalability of hybrid rocket regression models is critical for the enlargement and commercialization of small-scale engines developed within universities and similar research institutions. This paper investigates the fuel regressi...
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Landon Kamps, Shota Hirai and Harunori Nagata
Hybrid rockets are attractive as post-boost stages and kick motors due to their inherent safety and low cost, but it is not clear from previous research which oxidizer is most suitable for maximizing ?V within a fixed envelope size, or what impact O/F sh...
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Landon Kamps, Kazuhito Sakurai, Yuji Saito and Harunori Nagata
Static firing tests of a hybrid rocket motor using liquid nitrous oxide (N2O) as the oxidizer and high-density polyethylene (HPDE) as the fuel are analyzed using a novel approach to data reduction that allows histories for fuel mass consumption, nozzle t...
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