solid rocket oxidizer
基本解释
- 固体火箭氧化剂
英汉例句
- 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。 - Results of subscale engine test show that the insulation (PFDH-2) can be used for heat protection of oxidizer rich solid rocket engine chamber.
试车结果表明，PFDH-2绝热层可以对富氧环境下工作的发动机燃烧室实施有效热防护。