Large-Scale CAMUI Type Hybrid Rocket Motor Scaling, Modeling, and Test Results
Abstract
<jats:p>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 regression rates of recent 40 kN thrust-class motor experiments, which were designed based on fuel regression rate correlations of 2.5 kN thrust-class motors from previous research. The results show that fuel regression rates of the 40 kN experiments were within 26% of predictions made using correlations based on 2.5 kN experiments.</jats:p>
Journal
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- Aerospace
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Aerospace 9 (1), 1-, 2021-12-21
MDPI AG
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Details 詳細情報について
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- CRID
- 1360857593711332352
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- ISSN
- 22264310
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- Data Source
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- Crossref
- KAKEN