改性双基推进剂燃烧催化规律的正交试验研究  

Study of Combustion Catalysis for Smokeless Modified Double Base Propellant

作　　者：潘文达[1] 常景湘[1] 季远芬 

机构地区：[1]西安近代化学研究所,西安710065

出　　处：《固体火箭技术》1998年第2期41-46,共6页Journal of Solid Rocket Technology

摘　　要：用正文试验法研究了无烟改性双基推进剂的催化剂炭黑、铜盐和铅盐对燃速和压强指数的影响，并用正交多项式求算了催化剂含量与燃速及压强指数的定量关系式。The effects of combustion catalysts, carbon blacr, copper salt and lead salt, on burning rate and pressure exponent of smoke1ess modified double base propellant (SMDBP) were investigated by the orthogonal test method. The quantitative re1ationships of the burning rate and pressure exponent with the content of the catalysts were derived using the orhtogonai multinomials.

关 键 词：改性双基推进剂 燃烧催化剂 正变试验 

分 类 号：V512.2[航空宇航科学与技术—航空宇航推进理论与工程]