固体火箭技术2001，Vol.24Issue(1)：68-72,5.
大长细比小型固体发动机后点火试验研究
Experimental Investigation of Aft-End Ignition for High Slenderness Ratio and Small-Size Solid Motor
摘要
Abstract
Ignition characteristic parameters and affecting factors of small-size solid propellant rocket motor is described. The design idea and test situation of aft-end ignition for high slenderness ratio,smallsize solid rocket motors with a tailpipe nozzle are introduced and summerized.关键词
固体推进剂火箭发动机/点火/后点火+分类
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屠小昌,张春英,万东,张建伟..大长细比小型固体发动机后点火试验研究[J].固体火箭技术,2001,24(1):68-72,5.
