少烟推进剂配方优化设计  

Optimization on Composition of Reduced Smoke Propellant

作　　者：彭培根[1] 张仁[2] 刘德辉[1] 王振芳[1] 彭网大[1] 

机构地区：[1]国防科技大学材料科学与应用化学系 [2]材国防科技大学料科学与应用化学系

出　　处：《国防科技大学学报》1993年第1期73-77,共5页Journal of National University of Defense Technology

摘　　要：本文报道了关于降低固体火箭发动机喷气羽烟对微波、激光制导信号的干扰和衰减的研究成果——一种少烟HTPB推进剂。它具有低压点火性能良好,燃烧稳定,能提高排气羽烟对微波和激光透过率三倍以上。In this paper, the research results of reducing interferences and attenuations of solid rocker motorexhaust plume to microwave and laser guidance signal have been reported. The results include: reducedsmoke HTPB propellants with good ignition properties at low pressure and good steadiness of combus-tions, which make the transmissivities of both microwave and laser to exhaust plumes increase by a fac-tor of 3.

关 键 词：少烟推进剂 优化设计 固体推进剂 

分 类 号：V512[航空宇航科学与技术—航空宇航推进理论与工程]