空空导弹发动机采用少烟复合固体推进剂评述  

A REVIEW FOR SMOKE-REDUCED COMPOSITE SOLID PROPELLANT APPLIED TO AIR-TO-AIR MISSILE ROCKET MOTORS

作　　者：蔡选义[1] 

机构地区：[1]航空航天部014中心

出　　处：《推进技术》1990年第4期71-73,共3页Journal of Propulsion Technology

摘　　要：本文在总结我国空空导弹发动机研制的基础上,分析空空导弹发动机尾喷流对载机的影响.同时,从导弹发动机设计的角度出发,根据国内实际水平,提出采用少烟复合固体推进剂作为今后减少尾喷流对载机影响的主要技术途径.Based on the development of air-to-air missile motors in our country, in this paper the effects on the fighter airplane of the air-to-air missile motor exhaust plume impingement are analyzed.Under the consideration on design of the missile motors and present technical level in our country.Smoke-reduced composite solid propellants are presented as the main technological way to reduce effects of exhaust plume impingement on fighter airplane.

关 键 词：火箭发动机 固体推进剂 空对空导弹 尾喷流 

分 类 号：TJ760.33[兵器科学与技术—武器系统与运用工程]