...电子领域权威资讯传媒 关键词：固体火箭发动机；冷流缩比试验；喷管摆动；试验方法 [gap=1096]Key words: solid-rocket engine； cold-flow testing of sub-scale model； swinging nozzle； test method ..
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Solid rocket engine case 固体火箭发动机壳体
liquid-solid rocket engine 液固火箭发动机 ; 固火箭发动机
Solid rocket engine 固体火箭发动机
Solid rocket engine test 固体火箭发动机试验
solid rocket engine shell 固体火箭发动机壳体
pulse solid rocket engine 脉冲固体火箭发动机
integral solid rocket engine 整体式固体火箭冲压发动机
Finite element software of ANSYS has been used for making a finite element analysis of a certain type of ball-socket nozzle's pendulous socket in solid-rocket engine.
本文应用an SY S有限元分析软件，完成了对某型号固体火箭发动机珠承喷管摆动接头的有限元分析。
The ablative property requirements and the studies on the insulation layer of solid rocket engine in oxidizer rich environment were presented.
介绍了富氧环境下固体火箭发动机对绝热层性能的要求，以及在该特殊条件下对绝热层所开展的研究工作。
The fault effects on restrict layer debonding and crack burning were studied by simulated test in order to provide analysis basis of fault diagnostics for solid rocket engine.
用模拟试验研究各种脱粘和裂缝燃烧对发动机造成的故障效应，为故障诊断和失效分析提供依据。
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