Cheng Tianze
Pitzer College, Claremont, CA, USA.
Des Monomers Polym. 2019 Mar 1;22(1):54-65. doi: 10.1080/15685551.2019.1575652. eCollection 2019.
Current solid rocket propellant formulations still employ traditional ingredients utilized since the 1960s, such as hydroxyl terminated polybutadiene (HTPB). Recent advances in energetic polymer see many binders capable of providing higher specific impulse and burn rates over HTPB. As shown by calculations, even slight increases in specific impulse can drastically increase the maximum payload of a launch system. Therefore, replacing HTPB with energetic binders could provide heavy space missions the needed extra boost. Energetic binders could also be paired with chlorine-free energetic oxidizers to synergistically provide a specific impulse exceedingly higher than the current formulation while reducing pollution. A comprehensive evaluation of the synthesis, mechanical properties, and performance of various trending and overlooked energetic polymers is described. Several outstanding candidates show promising properties to replace HTPB.
当前的固体火箭推进剂配方仍采用自20世纪60年代以来使用的传统成分,如端羟基聚丁二烯(HTPB)。高能聚合物的最新进展表明,许多粘合剂能够提供比HTPB更高的比冲和燃烧速率。计算表明,即使比冲略有增加,也能大幅提高发射系统的最大载荷。因此,用高能粘合剂取代HTPB可为重型太空任务提供所需的额外推力。高能粘合剂还可与无氯高能氧化剂配合使用,协同提供比当前配方高得多的比冲,同时减少污染。本文描述了对各种热门和被忽视的高能聚合物的合成、机械性能和性能的综合评估。几种优秀的候选物显示出有望取代HTPB的性能。