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- The fact proves that solid propellant could be possibly used as GDL fuel. 實(shí)驗結果表明，固體推進(jìn)劑可以 成為GDL燃料。
- The progress of the aging property of solid propellant were reviewed. 綜述了國內外推進(jìn)劑材料老化性能的研究進(jìn)展。
- A mass of solid propellant. 塊狀燃料一塊固體推進(jìn)劑
- Solid propellant engine systems are basically less flexible in operation than liquid or hybrid propellant systems. 固體推進(jìn)劑發(fā)動(dòng)機系統的可調性基本上比液體或混合型的要差。
- 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(guò)相當簡(jiǎn)單的推導來(lái)試圖闡明固體推進(jìn)劑火箭系統的某些優(yōu)缺點(diǎn)。
- So ADN is the first candidate oxidizer instead of AP in solid propellant in 21st century. 化學(xué)安定性和相容性滿(mǎn)足要求,故ADN將是21世紀首選的AP替代物。
- Herb Chelner,Jim Buswell,Dan evans.Embedded sensors for monitoring solid propellant grain. 余宏發(fā).;光纖傳感器在固體發(fā)動(dòng)機測試中的應用
- The pasty propellant is a new kind of chemical propellant derived from solid propellant. 膏體推進(jìn)劑是由固體推進(jìn)劑衍變而成的一種新型化學(xué)推進(jìn)劑。
- J.J. Choury,carbon/carbon materials for nozzle of solid propellant rocket motors[J].AIAA76-609. 崔紅;李瑞珍;蘇君明等.;多元基體抗燒蝕炭/炭復合材料的微觀(guān)結構分析[J]
- Studies the ignition mode of solid propellant processed with high-pressure waterjet. 研究固體推進(jìn)劑在高壓水射流作用下的點(diǎn)火模式。
- Using parabolic trajectory of ballistic missile,surface to air missile with solid propellant can realize the aim of lesser weight and farther range. 地空導彈采用彈道導彈的拋物彈道技術(shù)，能夠實(shí)現應用固體推進(jìn)劑達到低質(zhì)量遠射程的目標。
- The one-dimensional two-phase flow model of solid propellant electrothermal chemical gun (SPETCG) is established in the paper. 該文建立了固體工質(zhì)電熱化學(xué)炮（SPETCG）內彈道一維兩相流模型。
- Based on modified Arrhenius formula, an integral method and a two-step regression method for storage life prediction of solid propellant are presented. 摘要在修正的阿倫尼斯公式基礎上，提出固體推進(jìn)劑貯存壽命的整體預測方法和兩步回歸預測方法。
- The results of the experiments show that the technique is a rapid, effective method for the disbond detecting of solid propellant rocket motors. 實(shí)驗研究結果表明,該技術(shù)可對固體火箭發(fā)動(dòng)機鋼筒與絕熱層之間的脫粘作快速有效的檢測。
- Based on modified Arrhenius formula,an integral method and a two-step regression method for storage life prediction of solid propellant are presented. 在修正的阿倫尼斯公式基礎上,提出固體推進(jìn)劑貯存壽命的整體預測方法和兩步回歸預測方法。
- This pa per presents plume temperature measurements of a mounted solid propellant rocket engine measured using a 6-target 8-wavelength pyrometer. 對于固體火箭發(fā)動(dòng)機羽焰溫度的測量是困難的,了解其溫度分布對于研究發(fā)動(dòng)機內燃燒流場(chǎng)的特性有重要價(jià)值。
- The high-pressure combustion properties of NEPE high-energy solid propellant were simulated and calculated by using the GA-BP neural network. 針對計算需求,對NEPE類(lèi)高能固體推進(jìn)劑配方進(jìn)行了全新表征,提出了13個(gè)表征參數。
- The ground-launched missiles are fitted with tandem mounted solid propellant boost motor assemblies, which are jettisoned after use. 地基導彈使用前后安裝的固體火箭助推馬達, 使用后被拋棄。
- The randomness of parameters is bound to occur for solid propellant, because it is a type of particles-filled composite. 固體推進(jìn)劑是一種顆粒填充復合材料,其性能參數具有一定的分散性。
- Aiming at calculation requirement,NEPE high-energy solid propellant formulation was characterized,and 13 parameters were put forward. 燃速預示結果表明,該方法計算誤差小于10%25,精度較高,能指導高能固體推進(jìn)劑高壓燃燒性能研究及配方設計;
