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Aerospace, v.8 no.9, 2021년, pp.253 -
Kamps, Landon , Hirai, Shota , Nagata, Harunori
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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 ΔV within a fixed envelope size, or what impact O/F shift and nozzle erosion will have on &Del...
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Kamps, Landon, Hirai, Shota, Sakurai, Kazuhito, Viscor, Tor, Saito, Yuji, Guan, Raymond, Isochi, Hikaru, Adachi, Naoto, Itoh, Mitsunori, Nagata, Harunori. Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using Oxygen/High-Density Polyethylene. Journal of propulsion and power, vol.36, no.3, 423-434.
Ito, Seiji, Kamps, Landon, Nagata, Harunori. Fuel Regression Characteristics in Hybrid Rockets Using Nitrous Oxide/High-Density Polyethylene. Journal of propulsion and power, vol.37, no.2, 342-348.
Carmicino, Carmine, Sorge, Annamaria Russo. Role of Injection in Hybrid Rockets Regression Rate Behaviour. Journal of propulsion and power, vol.21, no.4, 606-612.
Nagata, Harunori, Teraki, Hayato, Saito, Yuji, Kanai, Ryuichiro, Yasukochi, Hiroyuki, Wakita, Masashi, Totani, Tsuyoshi. Verification Firings of End-Burning Type Hybrid Rockets. Journal of propulsion and power, vol.33, no.6, 1473-1477.
Saito, Yuji, Yokoi, Toshiki, Yasukochi, Hiroyuki, Soeda, Kentaro, Totani, Tsuyoshi, Wakita, Masashi, Nagata, Harunori. Fuel Regression Characteristics of a Novel Axial-Injection End-Burning Hybrid Rocket. Journal of propulsion and power, vol.34, no.1, 247-259.
Hitt, Matthew A., Frederick Jr., Robert A.. Testing and Modeling of a Porous Axial-Injection, End-Burning Hybrid Motor. Journal of propulsion and power, vol.32, no.4, 834-843.
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Saito, Yuji, Kimino, Masaya, Tsuji, Ayumu, Okutani, Yushi, Soeda, Kentaro, Nagata, Harunori. High Pressure Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rockets. Journal of propulsion and power, vol.35, no.2, 328-341.
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Kamps, Landon, Saito, Yuji, Kawabata, Ryosuke, Wakita, Masashi, Totani, Tsuyoshi, Takahashi, Yusuke, Nagata, Harunori. Method for Determining Nozzle-Throat-Erosion History in Hybrid Rockets. Journal of propulsion and power, vol.33, no.6, 1369-1377.
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