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- For one thing, they simplify the design of a rocket engine. 首先，它們可以簡化火箭發動機的設計。
- The rocket engine carries with it the oxygen of its own . 火箭發動機自帶氧氣。
- Mo nozzle for the rocket engine nozzle professional. 鉬噴嘴專業用於火箭發動機噴嘴。
- Armstrong and Aldrin fired the lander rocket engine. 阿姆斯特朗和奧爾德林點燃了登月艙的火箭發動機。
- Unlike a rocket engine, the jet engine, as you konw, is an "air breather" . 正如你們所知道的，這種噴氣發動機與火箭發動機不同：它是「空氣噴氣發動機。」
- Unlike a rocket engine, the jet engine, as you know, is an "air breather". 正如你們所知道的，這種噴氣發動機與火箭發動機不同：它是「空氣噴氣發動機」。
- The leak of Liquid Rocket Engine (LRE) is very common and dangerous. 液體火箭發動機的泄漏是常見和極其危險的故障。
- It had a rocket engine that the astronauts fired to begin circling the moon. 宇航員點燃服務艙的火箭發動機，可以開始繞月飛行。
- The feed system of a rocket engine may be the cause of undesirable oscillations. 火箭供應系統可能是有害的振源。
- With a tremendous roar from its rocket engine,the satellite is sent up into the sky. 隨著火箭發動機發出的巨大的轟鳴聲，衛星被送上了天空。
- Vortex injection provides a form of swirl or cyclone combustion for a rocket engine similar to systems often employed in industrial furnaces. 渦流噴射在火箭發動機中產生一種渦流或旋渦形式的燃燒，與工業爐中常採用的系統相似。
- With a tremendous roar from its rocket engine, the satellite is sent up into the sky. 隨著火箭發動機發出的巨大的轟鳴聲，衛星被送上了天空。
- A jet or rocket engine based on a form of aerodynamic propulsion in which the vehicle emits a high-speed stream. 基於空氣動力學的推進噴氣和火箭。
- The article studys the diffuser in the active injector altitude simulated test system of solid rocket engine. 對固體火箭發動機主動引射高空模擬試車系統中的擴壓器部分進行研究。
- The integrity test of Liquid Rocket Engine (LRE) must be carried out before its launch. 在液體火箭發動機發射前，必須進行完整性試驗。
- The article discusses the technology of kerosene supplying in the starting of LOX/kerosene rocket engine testing. 介紹了液氧/煤油發動機試驗起動過程中的煤油供應技術。
- Vacuum vessel seal structure used in the leak test of a liquid rocket engine turbopump is discussed. 論述了某型號液體火箭發動機渦輪泵高壓低溫靜密封檢漏試驗用真空室密封結構的設計問題。
- The craft may have its own small rocket engines for orienting and maneuvering. 該機器可以有它自己的小型火箭發動機來定位和發動。
- C6H15N and HNO3-27S can be used as hypergolic propellant in rocket engines. 三乙胺和硝酸-27S作為自燃推進劑可應用於火箭發動機中。
- This pattern obsturator can satisfy requirement of rocket engine on the interior ballistic and exterior ballistic. 文中結合閉氣裝置工作環境,對火箭發動機的閉氣裝置性能進行了分析。
