摘要
针对高能固体火箭推进剂使用储氢材料进行了分析,从金属氢化物、金属氮氢化合物以及金属配位氢化物这几方面着手,对储氢材料分解推进剂组分、改善燃烧性能等作用作了分析,然后对其在推进剂中的实际应用及发展前景作了阐述。
High energy solid rocket propellants were analyzed using a hydrogen storage material, begin from the metal hydride, metal hydrogen and nitrogen compounds, and metal hydride ligand in these areas, the decomposition of hydrogen storage materials propellant components improve the combustion performance an analysis of the role, and then elaborated on its practical application and development prospects in the propellant.
出处
《化工设计通讯》
CAS
2016年第2期52-52,55,共2页
Chemical Engineering Design Communications
关键词
储氢材料
高能固体火箭
推进剂
hydrogen storage material
high energy solid rocket
propellant
