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   静态点火试验 的翻译结果: 查询用时:0.337秒
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静态点火试验
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  相似匹配句对
     TESTING
     试验
短句来源
     STATIC CHARACTERISTICS TEST OF CONCRETE COMPOUND MATERIAL
     混凝土复合材料的静态试验研究
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     Static clearance checking test of metro vehicles
     地铁车辆的静态限界试验
短句来源
     Experiment Research to Multi-Points-Ignition Technology
     多点点火技术的试验研究
短句来源
     Experimental Study on Electronic Ignition System of Engine
     电子节能点火装置的试验研究
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  static firing
Static firing rates of premotor and primary motor cortical neurons associated with torque and joint position
      
From this relation it was calculated that at 25° C an elevation of 0.1 mmol/l external calcium above the control value (1.53 mmol/l) reduces static firing rate by 0.35 impulses per second.
      
Its initial testing was to have started this spring with a static firing at Vandenberg AFB, Calif.
      
Mounting stands and missile silos have been used for the static firing of rocket and missile motors for demilitarization.
      
Open burning and static firing have been used for the demilitarization of rocket and missile motors.
      
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This paper shows several p~t curves of static ignition test of base bleed units whichhave been analysed and researched,states various phenomenon during the process of the ign-ition of base bleed units.The igrition properties of the base bleed units have been concludedand the improving methods favourable to the ignition of base bleed units have been put for-ward.

本文对底排装药静态点火试验的p~t曲线,进行了分析研究.阐述了底排装药被点燃时发生的各种现象,规纳出装药的点燃特性,提出了一些有利于底排装药点燃的改进方向.

Abstract The effect of swirling on solid rocket motor performance is investigated analytically and expermentally.The investigation on burning rate sensitivity in detail is completed.The prediction programs of transient burning rate,steady state burning rate and internal ballistic performance are established,the calculation results are compared with the experimental data.The effect of propellant ingredients on the swirling solid motor performance is also...

Abstract The effect of swirling on solid rocket motor performance is investigated analytically and expermentally.The investigation on burning rate sensitivity in detail is completed.The prediction programs of transient burning rate,steady state burning rate and internal ballistic performance are established,the calculation results are compared with the experimental data.The effect of propellant ingredients on the swirling solid motor performance is also revealed.Through a series of researches,the following conclusions are reached:if the aluminium content of the propellant remains constant,the greater the diameter of aluminium particles,the higher the burning rate sensitivity;if the diameter remains constant,the greater the content,the higher the sensitivity.For a high burning rate propellant,there exist a higher threshold of acceleration and a lower burning rate sensitivity.For star grain motor,the effect of swirling flow on its internal ballistic performance is smaller,than in the motor with conocyl grain.The prediction results of the theoretical model are consistent with the experimental results.The theoretical model can be applied to engineering design.

本文介绍了远程火箭中间段制导地面动态联试用的大L*脉冲发动机内弹道性能实验研究的情况,包括静态点火试验、动态旋转试验和高低温环境试验的情况。试验数据与设计数据符合良好。试验结果表明,脉冲发动机的主要性能满足与弹上控制系统动态联试的要求,但也带有大L*发动机的某些明显特点。

 
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