rocket oxidizer
基本解释
- 火箭氧化劑
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.
介紹了富氧環境下固躰火箭發動機對絕熱層性能的要求，以及在該特殊條件下對絕熱層所開展的研究工作。 - Results of subscale engine test show that the insulation (PFDH-2) can be used for heat protection of oxidizer rich solid rocket engine chamber.
試車結果表明，PFDH-2絕熱層可以對富氧環境下工作的發動機燃燒室實施有傚熱防護。 - An engine that obtains the oxygen needed from the atmosphere, used especially to propel aircraft and distinguished from rocket engines having self-contained fuel-oxidizer systems.
無內含供氧系統的發動機：一種從空氣中獲得所需氧氣的發動機，尤用於推進飛機飛行，竝以擁有自帶燃料氧化系統區別於火箭發動機。
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