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3D printed hybrid rocket fuels with μAl core-shell particles coated with polyvinylidene fluoride and polydopamine:Enhanced combustion characteristics

Qihang Chen Xiaolong Fu Weitao Yang Suhang Chen Zhiming Guo Rui Hu Huijie Zhang Lianpeng Cui Xu Xia

防务技术2025，Vol.46Issue(4)：59-70,12.

防务技术2025，Vol.46Issue(4)：59-70,12.DOI:10.1016/j.dt.2024.12.002

3D printed hybrid rocket fuels with μAl core-shell particles coated with polyvinylidene fluoride and polydopamine:Enhanced combustion characteristics

Qihang Chen ¹Xiaolong Fu ¹Weitao Yang ¹Suhang Chen ²Zhiming Guo ³Rui Hu ¹Huijie Zhang ²Lianpeng Cui ²Xu Xia¹

作者信息

1. Xi'an Modern Chemistry Research Institute,Xi'an,710065,China
2. School of Chemical Engineering/Xi'an Key Laboratory of Special Energy Materials/Shaanxi University Key Laboratory of High-Energy Chemical Materials,Northwest University,Xi'an 710069,China
3. School of Mechatronics Engineering,North University of China,Taiyuan,030051,China
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摘要

关键词

Hybrid propulsion/Regression rate/3D print fuels/Micro aluminum/Core-shell/μAl@PDA@PVDF

Key words

Hybrid propulsion/Regression rate/3D print fuels/Micro aluminum/Core-shell/μAl@PDA@PVDF

引用本文复制引用

Qihang Chen,Xiaolong Fu,Weitao Yang,Suhang Chen,Zhiming Guo,Rui Hu,Huijie Zhang,Lianpeng Cui,Xu Xia..3D printed hybrid rocket fuels with μAl core-shell particles coated with polyvinylidene fluoride and polydopamine:Enhanced combustion characteristics[J].防务技术,2025,46(4):59-70,12.

基金项目

This research was funded by the National Natural Science Foundation of China(Grant No.06101213)and the National Natural Science Foundation of China(Grant No.22105160).It was per-formed using the combustion test equipment at the School of Chemical Engineering at Northwest University(NWU).We also thank Shiyanjia Lab(www.shiyanjia.com)for support during the DSC and TG test. （Grant No.06101213）

防务技术

ISSN：2214-9147

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