Analysis of influencing factors for variable thrust SRM during thrust regulating

被引:0
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作者
National Key Laboratory of Combustion, Flow and Thermo-Structure, The 41st Institute of the Fourth Academy of CASC, Xi'an, China [1 ]
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来源
Guti Houjian Jishu | / 4卷 / 475-479期
关键词
Assembly clearances - Field stabilization - Nozzle structure - Numerical results - Regulating characteristics - Thrust delay - Torsional moment - Variable thrust SRM;
D O I
10.7673/j.issn.1006-2793.2014.04.008
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