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Method for Determining Nozzle-Throat-Erosion History in Hybrid Rockets
Title: | Method for Determining Nozzle-Throat-Erosion History in Hybrid Rockets |
Authors: | Kamps, Landon Browse this author | Saito, Yuji Browse this author | Kawabata, Ryosuke Browse this author | Wakita, Masashi Browse this author →KAKEN DB | Totani, Tsuyoshi Browse this author →KAKEN DB | Takahashi, Yusuke Browse this author →KAKEN DB | Nagata, Harunori Browse this author →KAKEN DB |
Issue Date: | Nov-2017 |
Publisher: | The American Institute of Aeronautics and Astronautics |
Journal Title: | Journal of propulsion and power |
Volume: | 33 |
Issue: | 6 |
Start Page: | 1369 |
End Page: | 1377 |
Publisher DOI: | 10.2514/1.B36390 |
Abstract: | The authors of this paper introduce a new reconstruction technique titled nozzle-throat reconstruction technique to estimate nozzle-throat-erosion history and oxidizer-to-fuel-mass-ratio history in hybrid rockets. Nine static-firing tests were carried out on a 2kN-class cascaded multistage impinging-jet-type hybrid-rocket motor under varying oxidizer-flow rates to evaluate the accuracy of reconstructed results. Nozzle-throat-erosion histories calculated by the nozzle-throat reconstruction technique agreed well with measured values for initial nozzle-throat radius, and successfully reconstructed the case, in which no measurable amount of nozzle-throat erosion occurred. For equivalence ratios 0.6-1.4, the relationship between nozzle-throat-erosion rate and equivalence ratio of reconstructed results displays a trend consistent with chemical-kinetic-limited heterogeneous-combustion theory, as well as predictions made by previous researchers. |
Type: | article (author version) |
URI: | http://hdl.handle.net/2115/67733 |
Appears in Collections: | 工学院・工学研究院 (Graduate School of Engineering / Faculty of Engineering) > 雑誌発表論文等 (Peer-reviewed Journal Articles, etc)
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Submitter: Kamps Landon Thomas
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