P - propellant 中文

propellant n.推進物，推進劑；(槍炮的)發射火藥；噴氣燃料。 hi...

n. 推進物，推進劑；(槍炮的)發射火藥；噴氣燃料。 high-energy propellant 高能燃料。 work horse propellant 【火箭】通用燃料。 “propellant office propellant office“ 中文翻譯：推進劑室“aerosol propellant“ 中文翻譯：氣溶膠火箭燃料; 氣溶膠拋射劑; 氣溶膠噴射劑; 氣溶膠噴霧劑; 氣溶膠型噴射劑; 氣霧拋射劑“bi propellant“ 中文翻譯：雙推進劑“boron propellant“ 中文翻譯：含硼推進劑“boron-propellant“ 中文翻譯：含硼推進劑“butane propellant“ 中文翻譯：丁烷推進劑“cast propellant“ 中文翻譯：模鑄推進劑“charge; propellant“ 中文翻譯：推進劑藥柱“chemical propellant“ 中文翻譯：化學推進劑“chipping of propellant“ 中文翻譯：固體燃料的碎裂“colloidal propellant“ 中文翻譯：膠全推進劑; 膠態發放射藥; 膠態推進劑; 膠體推進劑“composite propellant“ 中文翻譯：復合推進劑; 混合推進劑; 組合燃料“cool propellant“ 中文翻譯：冷態發射劑“cryogenic propellant“ 中文翻譯：低溫火箭燃料; 低溫噴氣發動機燃料“density of propellant“ 中文翻譯：推進劑密度“gas propellant“ 中文翻譯：氣體推進劑“gaseous propellant“ 中文翻譯：氣體燃料; 氣體推進劑“gaseous-propellant“ 中文翻譯：氣體燃料; 氣體推進劑“hot propellant“ 中文翻譯：熱態發射劑“hybrid propellant“ 中文翻譯：固體液體燃料; 混合燃料; 混合推進劑“hypergolic propellant“ 中文翻譯：自然推進劑; 自燃推進劑“kerosine propellant“ 中文翻譯：煤油噴氣燃料“liquid propellant“ 中文翻譯：液體火箭燃料; 液體燃料; 液體推進劑“missile propellant“ 中文翻譯：火箭推進劑“propellant atomization“ 中文翻譯：推進劑霧化“propeling equipment control“ 中文翻譯：推進裝置控制

propellent
Effect of solid rocket propellants well - washing equipment 固體火箭旋噴洗井器洗井效果分析
Propellant actuated fixing equipement . tests 推進力控制的安裝設備.試驗
Aerosol air freshener with lpg and or dme as propellants 空氣清新氣霧劑
Space systems - fluid characteristics - hydrogen propellant 航天系統.流體特性.氫推進劑
Nomenclature of composite solid propellant and charge 復合固體推進劑及裝藥術語
When liquid propellants are used the fuel and oxidize are fed under pressure to one or more combustion chambers and expanded to atmosphere through convergent-divergent nozzles . 當使用液體推進劑時，在壓力作用下，燃料和氧化劑輸送到一個或幾個燃燒室中，并通過收斂-打散噴管，排到大氣中。
The mechanical properties of improved double-base propellants enabled one to envisage grain geometrics with large combustion areas and consequently high thrusts . 經過改進的雙基推進劑的機械性能使我們能夠指望獲得大燃燒面的藥柱幾何形狀，從而得到大推力。
The above discussion on first-stage propellant slosh effects is based on the saturn vehicles, which use kerosene for fuel and lox for oxidizer . 上面對于第一級推進劑晃動影響的討論，是建立在“土星”飛行器的基礎上，它是采用煤油做燃燒劑，液氧做氧化劑。
To appreciate the unsteady environment existing in liquid propellant rocket chambers it is necessary that the steady state be well understood . 為了分析液體推進劑火箭發動機燃燒室中存在的非穩態環境，必須很好地了解穩態狀態。
The dynamic aspects of the combustion process are determined primarily by the injection pattern, the propellant combination, and the operating conditions . 燃燒過程的動力特性主要由噴射型式，推進劑組合及工作條件來確定。
The time lag can be envisioned as the time required for the liquid propellants to travel from the injector to an effective combustion “front. “ 可以把遲滯想象為液體推進劑從噴注器運行到有效燃燒“鋒”所需的時間。
We shall try by means of a highly simplified development to expose certain advantages and disadvantages of solid propellant rocket systems . 我們想通過相當簡單的推導來試圖闡明固體推進劑火箭系統的某些優缺點。
The propellants are acceptable for military purposes as relates to surveillance, electrostatic sensitivity and friction sensitivity . 就監視安定度，靜電感度和摩擦感度而言，這些推進劑是可作為軍用的。
The application of a pressure difference across an injector does not cause an immediate velocity response of the liquid propellant . 經過噴注器的壓降發生變化時并不馬上引起液體推進劑速度變化。
Sampling of propellants under typical operating conditions may be necessary to obtain valid capacitance information . 為了獲得有效的容量資料，在典型的工作條件下對推進劑取樣是很必要的。
It is difficult to separate the effects on stability of the propellant properties from those of the injection scheme . 要把推進劑性質對穩定性的影響與噴射型式的影響分開是困難的。
In this domain, flames are observed to move about on the surface of the propellant in a manner that is too irregular . 在這一區間內，火焰在推進劑表面上的運動方式是如此的不規律。
In using eq. 3-1 of course one first identifies the fuel molecules and the oxidizer molecules of the propellant . 當然，應用式（3-1）時首先要辨明推進劑的燃燒分子及氧化劑分子。
Solid propellant engine systems are basically less flexible in operation than liquid or hybrid propellant systems . 固體推進劑發動機系統的可調性基本上比液體或混合型的要差。

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propellant

propellant n.推進物，推進劑；(槍炮的)發射火藥；噴氣燃料。 hi...

propellent

Effect of solid rocket propellants well - washing equipment 固體火箭旋噴洗井器洗井效果分析

Propellant actuated fixing equipement . tests 推進力控制的安裝設備.試驗

Aerosol air freshener with lpg and or dme as propellants 空氣清新氣霧劑

Space systems - fluid characteristics - hydrogen propellant 航天系統.流體特性.氫推進劑

Nomenclature of composite solid propellant and charge 復合固體推進劑及裝藥術語

The mechanical properties of improved double-base propellants enabled one to envisage grain geometrics with large combustion areas and consequently high thrusts . 經過改進的雙基推進劑的機械性能使我們能夠指望獲得大燃燒面的藥柱幾何形狀，從而得到大推力。

To appreciate the unsteady environment existing in liquid propellant rocket chambers it is necessary that the steady state be well understood . 為了分析液體推進劑火箭發動機燃燒室中存在的非穩態環境，必須很好地了解穩態狀態。

The dynamic aspects of the combustion process are determined primarily by the injection pattern, the propellant combination, and the operating conditions . 燃燒過程的動力特性主要由噴射型式，推進劑組合及工作條件來確定。

The time lag can be envisioned as the time required for the liquid propellants to travel from the injector to an effective combustion “front. “ 可以把遲滯想象為液體推進劑從噴注器運行到有效燃燒“鋒”所需的時間。

We shall try by means of a highly simplified development to expose certain advantages and disadvantages of solid propellant rocket systems . 我們想通過相當簡單的推導來試圖闡明固體推進劑火箭系統的某些優缺點。

The propellants are acceptable for military purposes as relates to surveillance, electrostatic sensitivity and friction sensitivity . 就監視安定度，靜電感度和摩擦感度而言，這些推進劑是可作為軍用的。

The application of a pressure difference across an injector does not cause an immediate velocity response of the liquid propellant . 經過噴注器的壓降發生變化時并不馬上引起液體推進劑速度變化。

Sampling of propellants under typical operating conditions may be necessary to obtain valid capacitance information . 為了獲得有效的容量資料，在典型的工作條件下對推進劑取樣是很必要的。

It is difficult to separate the effects on stability of the propellant properties from those of the injection scheme . 要把推進劑性質對穩定性的影響與噴射型式的影響分開是困難的。

In this domain, flames are observed to move about on the surface of the propellant in a manner that is too irregular . 在這一區間內，火焰在推進劑表面上的運動方式是如此的不規律。

In using eq. 3-1 of course one first identifies the fuel molecules and the oxidizer molecules of the propellant . 當然，應用式（3-1）時首先要辨明推進劑的燃燒分子及氧化劑分子。

Solid propellant engine systems are basically less flexible in operation than liquid or hybrid propellant systems . 固體推進劑發動機系統的可調性基本上比液體或混合型的要差。