Design of Liquid-Propellant Rocket Engines

被引：3
作者：
Partola, I. S.
机构：
来源：
JOURNAL OF MACHINERY MANUFACTURE AND RELIABILITY | 2012年 / 41卷 / 06期
关键词：
D O I：
10.3103/S1052618812060118
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
A design method for liquid-propellant rocket engines is proposed, on the basis of models adjusted in response to test results. This method increases the reliability of the results and reduces ground testing of the motors. The effectiveness of the method is confirmed by ground testing and flight experience with the motors developed by Salyut Design Bureau at Krunichev State Space-Research Center.
引用
收藏
页码：492 / 498
页数：7
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