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- Large Solid Propellant Booster Program 大型固体推进剂助推器计划
- solid propellant booster 固体燃料起飞发动机
- solid propellant boosters 助推器
- 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。
- 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。
- 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。
- 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。
- 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。
- 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。
- 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。
- 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 high-pressure combustion properties of NEPE high-energy solid propellant were simulated and calculated by using the GA-BP neural network. 针对计算需求,对NEPE类高能固体推进剂配方进行了全新表征,提出了13个表征参数。
