摘要
通过对导弹液体推进剂废液废水的组成和化学性质的分析,确定废液废水的处理方法。根据化学反应和实验结果确定处理剂的用量,分别对氧化剂和燃料废液废水的处理工艺进行了设计,并提出了防止大气污染、安全快速的有效处理措施。
Component and chemical character of liquid propellant wastes were analyzed,then the deposal technology was confirmed. The dosages of disposal reagents were calculated according to the chemical reaction and experimental data. The deposal flows of wastewater for nitro-oxidizer and fuel were designed respectively and some methods were actualized to avoid atmospheric pollution and to protect person security.
出处
《海军航空工程学院学报》
2010年第5期591-594,共4页
Journal of Naval Aeronautical and Astronautical University
关键词
化学法
红烟硝酸
混胺
航空燃油
chemical reaction
red-fuming nitric acid
mixed amines
aircraft fuel