gas rocket 中文意思是什麼

gas rocket 解釋
毒氣火箭
  • gas : n （pl gases ）1 氣，氣體，氣態 〈cf fluid; solid〉 2 可燃氣，煤氣，沼氣；【礦物】瓦斯。3 【軍事...
  • rocket : n 火箭；火箭彈，火箭發動機；火箭式投射器；〈英俚〉斥責。 a carrier [freight] rocket 載運火箭。 an...
  1. In a short time interval, a mass dm of gas is ejected from the rocket.

    在很短的時間內，由火箭噴射氣體的質量為dm
  2. Gas generator rocket can pressurize a high-pressure feed system.

    燃氣發生器能使高壓輸送系統增壓。
  3. It can be used not only to change the fire precision of the base bleed projectile, but also to improve the effect of reduction drag and expansion range. the calculating model of the secondary expansive pressure of the burning gas is constructed by means of analysis of the experimental resuits, it has been confirmed that the new base bleed unit can be designed, with the secondary expansive principle of the burning gas pressure. the engineering project of a hybrid base - bleed - rocket high - level efficient extended - range projectile is designed, with the secondary expansive principle of the burning gas pressure, the feasibility and the true worth of its engineering applications is validated in theory

    本文提出了底排燃氣壓力不隨外部壓力變化，既可改善底部彈射擊精度又可提高減阻效果的二次擴張原理，建立了底排燃氣二次擴張壓力的計算模型，並通過採用二次擴張原理的新型底排裝置與傳統底排裝置的對比試驗，驗證了新型底排裝置結構實現的可行性；完成了基於底排燃氣二次擴張高效增程原理的底排?火箭復合高效增程彈方案設計及其有關計算，從理論上驗證了其工程應用的可行性和實際價值。
  4. Aiming at the conveying - alcohol pipe system of a certin model gas generator in our school rocket engine field laboratory, this paper does a series of simulation studies using amesim, analyses and summarizes the results of simulations, and at the same time implements some waterhammer experiments, and compares the results with the ones of simulations

    本文針對我校火箭發動機試驗外場的某型燃發器試驗酒精供應管道系統，使用amesim進行了一系列的模擬研究，對模擬的結果進行了分析和總結，同時還開展了水擊試驗，並與模擬進行了對比。
  5. This paper described a cold gas simulation of solid rocket motor with submerged nozzle. a two - dimension model with rectangular channel was designed, which can simulate different flow conditions at three periods after ignition

    本文從冷流模擬的角度出發，設計了通道為矩形的含潛入噴管發動機冷流模型，可以模擬發動機工作過程中三個不同時刻的流動狀態。
  6. Part three raiders a game. crocodile left switches, oven gas bottle left in the switch, middle banana on the first rocket, the lower left - hand corner of machinery, machine screws below, the alligator left switch, gas bottle switch, the tail of a rocket, fired right lower antenna first

    第三集游戲攻略1 .鱷魚左邊的開關3次，烤爐左邊的煤氣瓶開關，中間的香蕉放在火箭頭處，左下角的機器，機器下面的螺絲，鱷魚左邊的開關，煤氣瓶開關，火箭尾部，右下天線發射頭。
  7. Introduction : insults a raiders game. clown nose, with the carousel next to the stick ltd. 528300 clown mouth, hydrogen gas bottles, of pink petals and children into the hands of the fire eat on the floor, on top of spring, ships cigarettes, trojan switch, put yellow balloons to sleepwalk, the lower left - hand corner of the rotary rocket

    第四集游戲攻略1 .小丑的鼻子，用旋轉木馬旁的棍子撐住小丑的嘴巴，氫氣瓶，將粉紅色的花瓣兒放到吃火人手下的地上，彈簧上方物，輪船的煙，木馬開關，把黃色的氣球給夢遊人，左下角旋轉的火箭。
  8. When the gas is made very hot inside the rocket, it will rush out of the end of the rocket, so it can make the rocket fly up into the sky

    當氣體在火箭里達到高溫的時候，它就會沖出火箭的尾部，因此就使火箭直上雲霄。
  9. In this paper, simple reacting flow model in solid - propellant ducted rocket combustor based on eddy break - up model is established. the model is used to simulate the three - dimensional combustion flowfields in an experimental motor. some factors how to affect the combustion efficiency are discussed in the paper, including air intake and gas generator nozzle

    本文基於簡單反應的旋渦分裂模型，建立了固體火箭沖壓發動機補燃室內的湍流燃燒模型，並在該模型下對某實驗發動機進行了三維數值模擬，研究了補燃室設計參數包括進氣道出口設計參數和燃氣發生器噴管設計參數對燃燒效率的影響。
  10. As the seat rode to the top of the rails, a port opened and gas ignited the rocket, blasting stricklin fully out of the cockpit like a roman candle

    彈射座椅滑行到導軌頂端時，出口被打通，氣體點燃，發動火箭推力裝置，象發射一座羅馬燭臺一樣把斯特里克林完全「炸」出駕駛艙。
  11. The gas supply system in the launch area offers compressed air 、 high - purity nitrogen and high - purity helium for carrier rocket 、 spacecraft test 、 fueling and satellite launch, which is an important part of the ground service support system in the launch area

    發射場配氣系統為運載火箭和衛星測試、加註、發射提供壓縮空氣、高純氮氣和高純氦氣，是發射場地面勤務系統的重要組成部分。
  12. In this way, supersonic fluid amplifier especially bistable valve with negative pressure switch is used in the rocket projectile thanks to its advantages of switching rapidly, the ability of low temperature air to control the high temperature gas and no moving parts in high temperature gas

    超音速射流雙穩閥，特別是採用負壓切換的超音速射流雙穩閥因其具有切換快速、可用低溫氣流控制高溫燃氣和在高溫燃氣中無活動部件的優點而適用於火箭彈的姿態控制系統中。
  13. Gas flow control techniquc of rocket ramjct is discussed, and then some base idea and research achievements in the design of that are also expressed in the paper

    對固體火箭沖壓發動機燃氣流量調節技術進行了論述，闡述了固體火箭沖壓發動機燃氣流量調節技術在設計上的一些基本思想及研究成果。
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