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- At first, the thermodynamic calculation of Solid Ducted Rocket is researche. 在此基础上,首先对固体冲压发动机热力计算展开了研究分析。
- The characterization of the combustion properties of the aluminum? magnesium fuel? rich propellant for unchoked ducted rocket was studied. 系统研究了铝镁贫氧推进剂低压燃烧特性的表征方法。
- 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。
- 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。
- 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]
- In this paper, the theory of minitype Solid Ducted Rocket with shot is researche nd analyzed. 本文研究和分析了炮射小型固体火箭冲压发动机的工作原理。
- It would be of great reference value for development of air-to-air missile propelled by integral solid ducted rocket. 对我国发展采用整体式固冲发动机的空空导弹具有重要的参考价值。
- The results of the experiments show that the technique is a rapid, effective method for the disbond detecting of solid propellant rocket motors. 实验研究结果表明,该技术可对固体火箭发动机钢筒与绝热层之间的脱粘作快速有效的检测。
- This pa per presents plume temperature measurements of a mounted solid propellant rocket engine measured using a 6-target 8-wavelength pyrometer. 对于固体火箭发动机羽焰温度的测量是困难的,了解其温度分布对于研究发动机内燃烧流场的特性有重要价值。
- The method developed in this paper can be used in the research field of the Ducted Rocket and fuel-rich propellant, to reduce the experimental cost effetely and shorten the research period greatly. 对于固体冲压发动机和贫氧推进剂的研制来说,本文研究的方法既可有效地降低试验成本,又可大大缩短研制周期,具有一定的工程应用价值。
- Mayer A E H J,Stowe R A.Experimental study into mixing in a solid fuel ducted rocket combustion chamber[R].AIAA 2000-3346. 余勇;陈小前;等.;三维实验固体火箭冲压发动机燃烧室湍流反应流数值模拟[J]
- Mayer A E H J,Stowe R A. Experimental Study Into Mixing in a Solid Fuel Ducted Rocket Combustion Chamber[R]. AIAA Paper 2000-3346. 张炜;夏智勋;姜春林;等.;新型非壅塞式固体火箭冲压发动机试验研究[J]
- 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 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。
- Using pintle technology, a conventional solid propellant rocket motor can provide variable thrust levels, increasing the energy utilizing efficiency and improving the capability of the missile. 喉栓式变推力发动机可实现固体火箭发动机的推力调节,提高能量利用效率,从多方面提升导弹武器的作战效能,因此具有强烈的军事需求。
- The compound solid propellant used by rocket engine is made of adhesive, oxidizer and some other additives.All of those are casted or extruded then solidified to form the propellant. 火箭发动机所使用的复合固体推进剂,是利用胶粘剂、氧化剂和其它添加剂等成分经浇注或挤出后,固化而成的固体药柱。
- Stowe R A, Champlain A De, Mayer A E H J. Modeling combustor performance of a ducted rocket[R]. AIAA paper 2000-3728. 张炜;方丁酉;夏智勋;等.;非壅塞固体火箭冲压发动机工作特性研究[J]
- Stowe R A,Champlain A D,Mayer A E H J.Modelling combustor performance of a ducted rocket[R].AIAA 2000-3728. 陈林泉;毛根旺;霍东兴;等.;燃气喷射方式对冲压发动机补燃室掺混效果的影响[J]
- 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。