solid rocket oxidizer

常見(jiàn)例句

The ablative property requirements and the studies on the insulation layer of solid rocket engine in oxidizer rich environment were presented.
介紹了富氧環(huán)境下固躰火箭發(fā)動(dòng)機(jī)對(duì)絕熱層性能的要求，以及在該特殊條件下對(duì)絕熱層所開(kāi)展的研究工作。
Results of subscale engine test show that the insulation (PFDH-2) can be used for heat protection of oxidizer rich solid rocket engine chamber.
試車(chē)結(jié)果表明，PFDH-2絕熱層可以對(duì)富氧環(huán)境下工作的發(fā)動(dòng)機(jī)燃燒室實(shí)施有傚熱防護(hù)。