Yuan Zhifeng, Yang Su-Lan, Zhao Fengqi, Liu Linlin, Zhang Ming, Wang Ying, Zheng Wei, Pei Jiangfeng, Hu Songqi
National Key Laboratory of Solid Rocket Propulsion, Northwestern Polytechnical University, Xi'an 710072, China.
Xi'an Modern Chemistry Research Institute, Xi'an 710065, China.
Langmuir. 2024 Dec 31;40(52):27228-27237. doi: 10.1021/acs.langmuir.4c02902. Epub 2024 Dec 4.
In this paper, a series of insensitive smokeless nitrocellulose (NC)-based propellants were prepared through the absorption rolling method. Their thermal stability was rigorously assessed via vacuum stability test (VST), and their thermal reactivity of the propellant was comprehensively investigated and compared using the thermogravimetric analysis (TG)/differential scanning calorimetry (DSC) technique. Additionally, the combustion characteristics were meticulously analyzed by a constant-volume combustion diagnosis system. The experimental results showed that the thermal stability of the propellant was significantly enhanced when -butyl--nitratoethyl nitramine (Bu-NENA) was used to partially or fully replace nitroglycerin (NG). However, an increase in Bu-NENA content corresponded with a decrease in the burning rate of the propellant. The catalytic effects observed in propellants varied markedly, influencing the composition of the products formed during thermal decomposition. Specifically, substituting 50 and 100% of NG with Bu-NENA resulted in reductions in the decomposition heat release of 96.2 and 258 J·g, respectively. Furthermore, the introduction of the catalyst significantly increased the burning rate under low-pressure conditions. For instance, at 2 MPa, the burning rate of Bu-0503 increased from 1.78 to 5.23 mm·s. A lower content of Bu-NENA was associated with a more luminous flame, while substituting 50 and 100% of NG with Bu-NENA led to decreases in flame temperature by 222 and 535 °C, respectively. The observed decrease in the flame temperature is attributed to the heat absorption during the volatilization of Bu-NENA, leading to a reduction in the thermal feedback of the flame.
在本文中,通过吸收滚压法制备了一系列基于不敏感无烟硝化纤维素(NC)的推进剂。通过真空稳定性测试(VST)严格评估了它们的热稳定性,并使用热重分析(TG)/差示扫描量热法(DSC)技术对推进剂的热反应性进行了全面研究和比较。此外,通过定容燃烧诊断系统对燃烧特性进行了细致分析。实验结果表明,当使用丁基-二硝基乙基硝胺(Bu-NENA)部分或完全替代硝化甘油(NG)时,推进剂的热稳定性显著提高。然而,Bu-NENA含量的增加对应着推进剂燃烧速率的降低。推进剂中观察到的催化作用变化显著,影响热分解过程中形成的产物组成。具体而言,用Bu-NENA替代50%和100%的NG分别导致分解热释放降低96.2和258 J·g。此外,催化剂的引入在低压条件下显著提高了燃烧速率。例如,在2 MPa时,Bu-0503的燃烧速率从1.78增加到5.23 mm·s。较低含量的Bu-NENA与更明亮的火焰相关,而用Bu-NENA替代50%和100%的NG分别导致火焰温度降低222和535°C。观察到的火焰温度降低归因于Bu-NENA挥发过程中的吸热,导致火焰的热反馈减少。