Effects of Different Metal Fuels on the Characteristics for HTPB-based Fuel Rich Solid Propellants

Pang Weiqiang; Fan Xuezhong; Zhao Fengqi; Xu Huixiang; Zhang Wei; Yu Hongjian; Li Yonghong; Liu Fangli; Xie Wuxi; Yan Ning

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Effects of Different Metal Fuels on the Characteristics for HTPB-based Fuel Rich Solid Propellants

机译：不同金属燃料对HTPB基富燃料固体推进剂性能的影响

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The microstructures and granularity distribution of different metal particles were investigated and the energy, sensitivity, and combustion properties of fuel rich solid propellants with different metal particles were studied in detail. It was found that the magnesium particles are more uniform than other metal powders, the mean diameter of the magnesium particles d(50)=67.6m is much higher than those of the other ones, which are in the range of 7.1m

机译：研究了不同金属颗粒的微观结构和粒度分布，并详细研究了不同金属颗粒的富燃料固体推进剂的能量，灵敏度和燃烧性能。发现镁颗粒比其他金属粉末更均匀，镁颗粒的平均直径d（50）= 67.6m远远大于其他金属颗粒，其范围在7.1m

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来源
《Propellants, Explosives, Pyrotechnics》 |2013年第6期|共8页
作者
Pang Weiqiang; Fan Xuezhong; Zhao Fengqi; Xu Huixiang; Zhang Wei; Yu Hongjian; Li Yonghong; Liu Fangli; Xie Wuxi; Yan Ning;
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正文语种 eng
中图分类爆炸物工业、火柴工业;
关键词
Material chemistry; Fuel-rich solid propellant; Metal fuels; Burning rate; Sensitivity;

机译：材料化学;富油固体推进剂;金属燃料;燃烧率;灵敏度;

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1. Effects of Different Metal Fuels on the Characteristics for HTPB-based Fuel Rich Solid Propellants [J] . Pang Weiqiang, Fan Xuezhong, Zhao Fengqi, Propellants, Explosives, Pyrotechnics . 2013,第6期

机译：不同金属燃料对HTPB基富燃料固体推进剂性能的影响
2. Experimental and numerical study of a full-size direct-connect dual-inlet DRE with a fuel-rich metalized solid propellant [J] . Zhu Min, Chen Xiong, Zhou Chang-sheng, International Journal of Heat and Mass Transfer . 2019,第Sepa期

机译：具有富含燃料金属化固体推进剂的全尺寸直接连接双口腔DRE的实验和数值研究
3. Metallised Fuel rich Propellants for Solid Rocket Ramjet: A Review [J] . B. K. Athawale, S. N. Asthana, Haridwar Singh Defence science journal . 2013,第4期

机译：用于固体火箭冲压发动机的金属化富油推进剂：综述
4. EFFECT OF COMPOSITION ON THETHERMOCHEMICAL CHARACTERISTICS OF METALIZED AND NON-METALIZED FUEL-RICH COMPOSITE PROPELLANTS [C] . HANY N. AMIN, SHOKRY A. SHOKRY, EL-SYED S. NASR, Energetic Materials: Processing and Product Design . 2008

机译：组成对金属化和非金属化富油复合推进剂热化学特性的影响
5. Regression rate and pyrolysis behavior of HTPB-based solid fuels in a hybrid rocket motor. [D] . Chiaverini, Martin John. 1997

机译：混合火箭发动机中基于HTPB的固体燃料的回归速率和热解行为。
6. Emission characteristics for polycyclic aromatic hydrocarbons from solid fuels burned in domestic stoves in rural China [O] . Guofeng SHEN, Shu TAO, Yuanchen Chen, -1

机译：中国农村家庭炉灶中燃烧的固体燃料中多环芳烃的排放特性
7. The effects of metallized fuel composition on the combustion characteristics of solid fuel ramjets. [O] . Karadimitris Adonis 1986

机译：金属化燃料成分对固体燃料冲压发动机燃烧特性的影响。

Effects of Different Metal Fuels on the Characteristics for HTPB-based Fuel Rich Solid Propellants

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