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- The fact proves that solid propellant could be possibly used as GDL fuel. 实验结果表明,固体推进剂可以 成为GDL燃料。
- The effects of TMOs and their mixtures on the burning rate and the pressure exponent of the aluminum magnesium fuel rich propellant for unchoked ducted rocket are investigated. 研究了过渡金属氧化物(TMO)及其复配物对非壅塞固体火箭冲压发动机铝镁贫氧推进剂燃烧特性的影响。
- The fuel rich propellant used for the unchoked ram rocket should has high burning rate exponent, appropriate burning rate, low flammability limit and steady combustion properties. 分析结果表明:非壅塞式固体火箭冲压发动机要求贫氧推进剂具有高的燃速压强指数、低的可燃极限和足够好的燃烧稳定性。
- The pyrolysis behavior of the fuel rich propellant based on boron was analysed and researched by thermalgravimetry analyse (TGA) and differential scanning calorimeter (DSC). 摘要用差示扫描量热(DSC)和热重分析法(TGA),分析、研究了含硼富燃料推进剂的热分解特性;
- The thermal decomposition characteristics of GAP simulated low oxygen fuel rich propellant were studied by using DSC method. The effect of TMO catalysts on the thermal decomposition characteristics is investigated in this paper. 采用 DSC方法研究了 GAP模拟贫氧推进剂的常压热分解特性 ,同时考察了 TMO催化剂对 GAP模拟贫氧推进剂热分解特性的影响。
- The progress of the aging property of solid propellant were reviewed. 综述了国内外推进剂材料老化性能的研究进展。
- A mass of solid propellant. 块状燃料一块固体推进剂
- Solid propellant engine systems are basically less flexible in operation than liquid or hybrid propellant systems. 固体推进剂发动机系统的可调性基本上比液体或混合型的要差。
- Using fine diameter boron, coating boron and adding other ingredient into the boron based fuel rich propellants can increase employed efficiency of boron. 指出硼表面的氧化物是造成硼点火困难和燃烧效率低的主要因素;
- We shall try by means of a highly simplified development to expose certain advantages and disadvantages of solid propellant rocket systems. 我们想通过相当简单的推导来试图阐明固体推进剂火箭系统的某些优缺点。
- The effect of different pulverized coals and chars on NO heterogeneous reduction in the fuel rich stage of reburning was studied in a bench scale flow reactor. 在小型流动反应器中研究了不同煤粉及其煤焦对富燃料再燃区NO异相还原的影响。
- So ADN is the first candidate oxidizer instead of AP in solid propellant in 21st century. 化学安定性和相容性满足要求,故ADN将是21世纪首选的AP替代物。
- This paper presents a new concept that particle concentration enrichment process through deceleration and diffusion process is the basis of fuel rich combustion technology. 提出了颗粒的滞止浓缩过程与弥散过程是浓缩煤粉燃烧技术的基础这一新概念,并分析了滞止浓缩过程与弥散过程的原理。
- Herb Chelner,Jim Buswell,Dan evans.Embedded sensors for monitoring solid propellant grain. 余宏发.;光纤传感器在固体发动机测试中的应用
- The pasty propellant is a new kind of chemical propellant derived from solid propellant. 膏体推进剂是由固体推进剂衍变而成的一种新型化学推进剂。
- J.J. Choury,carbon/carbon materials for nozzle of solid propellant rocket motors[J].AIAA76-609. 崔红;李瑞珍;苏君明等.;多元基体抗烧蚀炭/炭复合材料的微观结构分析[J]
- Studies the ignition mode of solid propellant processed with high-pressure waterjet. 研究固体推进剂在高压水射流作用下的点火模式。
- Using parabolic trajectory of ballistic missile,surface to air missile with solid propellant can realize the aim of lesser weight and farther range. 地空导弹采用弹道导弹的抛物弹道技术,能够实现应用固体推进剂达到低质量远射程的目标。
- The one-dimensional two-phase flow model of solid propellant electrothermal chemical gun (SPETCG) is established in the paper. 该文建立了固体工质电热化学炮(SPETCG)内弹道一维两相流模型。
- Based on modified Arrhenius formula, an integral method and a two-step regression method for storage life prediction of solid propellant are presented. 摘要在修正的阿伦尼斯公式基础上,提出固体推进剂贮存寿命的整体预测方法和两步回归预测方法。