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倒置喷管发动机性能测定方法的比较与分析
引用本文:毛根旺,陈福连,牛嵩高,吴建政.倒置喷管发动机性能测定方法的比较与分析[J].推进技术,1995,16(3):26-29.
作者姓名:毛根旺  陈福连  牛嵩高  吴建政
作者单位:西北工业大学航天工程学院
摘    要:采用三种试验方案对喷管倒置150°引起的比冲损失进行了测定、分析和比较。结果表明,双室串并发动机顺倒置四喷管引起的比冲相对损失为1.8%左右;如果将顺置采用单喷管,那么该项损失大约为4.1%。采用双室串并发动机时,测试系统和判读系统误差不能进入测试数据中,所以它比单独采用顺置和倒置时测定的数据可靠。

关 键 词:固体推进剂  火箭发动机  喷管

COMPARISON AND ANALYSES ON DETERMINING METHODS FOR PROPERTIES OF INVERSE NOZZLE ROCKET MOTORS
Mao Genwang,Chen Fulian,Niu Songgao and Wu Jianzheng.COMPARISON AND ANALYSES ON DETERMINING METHODS FOR PROPERTIES OF INVERSE NOZZLE ROCKET MOTORS[J].Journal of Propulsion Technology,1995,16(3):26-29.
Authors:Mao Genwang  Chen Fulian  Niu Songgao and Wu Jianzheng
Abstract:he loss of impulses caused by inverse nozzles with 150° has been determined, analyzed and compared through three kinds of tests. It turns out that the relative loss of impulses caused by common and inverse 4 nozzles in double-chamber series-parallel rocket motors is about 1. 8 %. When a single nozzle was used in solid rocket motors with common nozzle, the loss would be about 4. 1%. Since the errors of measuring and deciding systems can not be led into measurement data, determined data is more reliable than those determined by single common and inverse nozzles, when double-chamber series-parallel rocket motors are used.
Keywords:Solid propellant rocket engine  Engine nozzle  Nozzle efficiency  
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