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07:58 min
January 18, 2021
DOI:
10.3791/61555-v
提出了一种利用固体燃料颗粒与新型嵌套级级结构技术,提高混合火箭发动机的燃烧性能。
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Wang, Z., Lin, X., Li, F., Zhang, Z., Yu, X. Improving the Combustion Performance of a Hybrid Rocket Engine using a Novel Fuel Grain with a Nested Helical Structure. J. Vis. Exp. (167), e61555, doi:10.3791/61555 (2021).
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