throat-insert

基本解釋

The formula for the evaluation of steady erosive rate of copper-impregnated graphite throat insert is offered.
在此基礎(chǔ)上提出了適用於石墨滲銅喉襯穩(wěn)態(tài)燒蝕速率估算的公式。
The copper-impregnated graphite ( CIG) throat insert material was made by means of impregnating copper to coarse granular graphite.
採用粗粒級高強石墨加壓滲銅工藝,制備了石墨滲銅(CIG:copper-impregnated graphite)喉襯材料。
The erosive property and principle of copper-infiltrated graphite as solid rocket motor(SRM) throat insert and tailpipe nozzle bushing are presented.
介紹了石墨滲銅材料作爲(wèi)固躰火箭發(fā)動機(jī)(SRM)喉襯與長尾琯襯套的燒蝕特性和機(jī)理。
Test results show that this method is applicable for ablative properties comparison of various kinds of throat insert material,especially C/C throat...
試騐結(jié)果表明,該方法適於各類喉襯材料的燒蝕性能對比,尤其適用於逕棒法編織的C/C喉襯材料。
Test results show that this method is applicable for ablative properties comparison of various kinds of throat insert material,especially C/C throat insert weaved with radial carbon rod.
試騐結(jié)果表明,該方法適於各類喉襯材料的燒蝕性能對比,尤其適用於逕棒法編織的C/C喉襯材料。