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International Journal of Energetic Materials and Chemical Propulsion
Редактор-основатель: Kenneth K. Kuo (open in a new tab)

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ISSN Печать: 2150-766X

ISSN Онлайн: 2150-7678

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REACTIVITY AND COMBUSTION OF POROUS SILICON ENERGETIC CHIPS

Том 19, Выпуск 2, 2020, pp. 113-124
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2020027942
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Ruiqi Shen
Nanjing University of Science and Technology
Fei Ji
Institute of Space Propulsion, School of Chemical Engineering, Nanjing University of Science and Technology, Nanjing, 210094, China
Shouxu Wang
Institute of Space Propulsion, School of Chemical Engineering, Nanjing University of Science and Technology, Nanjing, 210094, China
Wei Zhang
Institute of Space Propulsion, School of Chemical Engineering, Nanjing University of Science and Technology, Nanjing, 210094, China
Yinghua Ye
Institute of Space Propulsion, School of Chemical Engineering, Nanjing University of Science and Technology, Nanjing, 210094, China

Краткое описание

Porous silicon (PS) is a three-dimensional nanostructured fuel. When an oxidant is filled into the porous structures of PS, it will become an energetic material. In the paper, a nanostructured PS energetic material filled by sodium perchlorate (NaClO4) and its energetic chips were fabricated by the electrochemical process, the oxidant deposition process, and the microelectromechanical system (MEMS) fabrication process. The differential scanning calorimetry results show that PS/NaClO4 decomposition reaction happens from 525.8°C to 574.3°C, and the released heat is about 689.5 J/g. The igniting delay time of energetic porous silicon/Cr bridge depends on the igniting voltage and the burning rate, and the combustion efficiency of PS chip depends on the ignition energy from the integrated Cr igniting bridge. The PS thrusters were fabricated by the MEMS process. The nozzle efficiencies of impulse were analyzed by the experiment. The experimental results show the convergent-divergent nozzle thruster is the best, and the straight nozzle thruster is better than no nozzle thruster.

Ключевые слова: energetic porous silicon, microigniter, microthruster, ignition, propulsion
ЛИТЕРАТУРА

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ЦИТИРОВАНО В

  1. Zhang Xiandie, Cui Rui, Mao Huiqing, Zhang Chun, Zhu Ying, Zhou Xiang, Effects of doping type of Si on the exothermic characteristics of Si/PTFE energetic composites, Journal of Thermal Analysis and Calorimetry, 2022. Crossref

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