Xie Ruiling, Li Hongyang, Li Hong, Zeng Shentao, Du Lixiaosong, Cai Qing, Shi Sujun, Xu Wenqi, Wang Ran, Luo Cui, Liu Ying
School of Materials, Beijing Institute of Technology, Beijing, China.
Shanghai Aerospace Control Technology Institute, Shanghai, China.
Phys Chem Chem Phys. 2025 Jun 18;27(24):13083-13090. doi: 10.1039/d5cp01213a.
Based on the aqueous sol-gel method, three types of nano-FeO particles with different microstructures were synthesized with FeSO solution as the precursor. The structural characteristics of these FeO particles and their effects on the high-temperature thermal decomposition of ammonium perchlorate (AP) and the combustion performance of AP/aluminum (Al) composite fuels were analyzed with scanning electron microscopy (SEM), energy dispersive spectroscopy (EDS), X-ray diffraction (XRD), surface area analysis, differential scanning calorimetry (DSC), and high-speed imaging. The results indicate that at a pH of 8, the synthesized nanoparticles comprise bulk and fibrous particles with an average particle size of approximately 70 nm, exhibiting some degrees of agglomeration. As the pH increases, the particle size shows a growing trend, with a gradual reduction in the quantity of fibrous particles. At a pH of 12, the morphology of the synthesized nanoparticles is predominantly bulk, characterized by an average particle size of 80 nm and no significant agglomeration; the bulk particles are identified as FeO, while the fibrous particles are FeOOH. With increasing pH, the specific surface area of the samples exhibits a decreasing trend, with no significant differences in specific surface area observed between the samples prepared at pH 10 and pH 12. The addition of three different sets of FeO nanoparticles led to a noticeable reduction in the high-temperature decomposition peak temperatures of AP, which decreased to 363.82 °C, 389.46 °C, and 404.54 °C, corresponding to reductions of 89.2 °C, 63.56 °C, and 48.48 °C, respectively; no significant differences were observed in the low-temperature decomposition peak temperatures. The heat release of the samples was measured at 635.56 J g, 1040.66 J g, and 985.34 J g, showing improvements of 60.08 J g, 465.18 J g, and 409.86 J g over pure AP. The maximum weight loss rates for the three samples were recorded at 363.91 °C, 388.76 °C, and 401.13 °C, corresponding to 69.1% min, 18% min, and 14% min. The combustion process of the composite fuels was divided into five stages: ignition, flaming, steady burning, decay, and extinguishment. The ignition delay time of composite fuels containing the nano-FeO catalyst decreased as the content of nano-FeO increased from 0.5 wt% to 1 wt% and 2 wt%, decreasing to 130 ms, 114 ms, and 95 ms, respectively, compared to reductions of 2 ms, 18 ms, and 37 ms for the composite fuel without nano-FeO. With the increased addition of nano-FeO particles, both the flame height and width during the steady burning stage increased significantly, resulting in a substantial enhancement of combustion duration. When the addition of nano-FeO reached 1 wt%, further increases in the particle content resulted in a stabilization of the flame area with no significant increases. Employing nano-FeO as a catalyst effectively enhances the combustion efficiency of composite fuels using AP as an oxidizer, suggesting good application prospects for nano-FeO particles as catalysts in solid rocket propellants.
基于水溶胶-凝胶法,以硫酸亚铁溶液为前驱体合成了三种具有不同微观结构的纳米FeO颗粒。采用扫描电子显微镜(SEM)、能谱仪(EDS)、X射线衍射仪(XRD)、比表面积分析仪、差示扫描量热仪(DSC)和高速成像技术,分析了这些FeO颗粒的结构特征及其对高氯酸铵(AP)高温热分解和AP/铝(Al)复合燃料燃烧性能的影响。结果表明,在pH值为8时,合成的纳米颗粒由块状和纤维状颗粒组成,平均粒径约为70 nm,呈现出一定程度的团聚。随着pH值的增加,粒径呈增长趋势,纤维状颗粒数量逐渐减少。在pH值为12时,合成的纳米颗粒形态以块状为主,平均粒径为80 nm,无明显团聚;块状颗粒为FeO,纤维状颗粒为FeOOH。随着pH值的增加,样品的比表面积呈下降趋势,在pH值为10和pH值为12制备的样品之间,比表面积无显著差异。添加三组不同的纳米FeO颗粒导致AP的高温分解峰值温度显著降低,分别降至363.82℃、389.46℃和404.54℃,相应降低了89.2℃、63.56℃和48.48℃;低温分解峰值温度无显著差异。样品的热释放量分别为635.56 J/g、1040.66 J/g和985.34 J/g,比纯AP分别提高了60.08 J/g、465.18 J/g和409.86 J/g。三个样品的最大失重率分别记录在363.91℃、388.76℃和401.13℃,分别为69.1%/min、18%/min和14%/min。复合燃料的燃烧过程分为五个阶段:点火、火焰燃烧、稳定燃烧、衰减和熄灭。含纳米FeO催化剂的复合燃料的点火延迟时间随着纳米FeO含量从0.5 wt%增加到1 wt%和2 wt%而减少,分别降至130 ms、114 ms和95 ms,相比不含纳米FeO的复合燃料分别减少了2 ms、18 ms和37 ms。随着纳米FeO颗粒添加量的增加,稳定燃烧阶段的火焰高度和宽度均显著增加,导致燃烧持续时间大幅延长。当纳米FeO的添加量达到1 wt%时,颗粒含量的进一步增加导致火焰面积稳定,无显著增加。采用纳米FeO作为催化剂可有效提高以AP为氧化剂的复合燃料的燃烧效率,表明纳米FeO颗粒作为固体火箭推进剂中的催化剂具有良好的应用前景。
Cochrane Database Syst Rev. 2025-6-9
ACS Appl Mater Interfaces. 2025-6-18
Cochrane Database Syst Rev. 2022-6-15
Cochrane Database Syst Rev. 2025-3-11
Heliyon. 2024-5-27
Cochrane Database Syst Rev. 2025-5-7