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低燃温
相关语句
  low burning temperature
    Research on Low Burning Temperature Mesa Double Base Propellant
    低燃温麦撒双基推进剂研究
  “低燃温”译为未确定词的双语例句
    he Performance of nonaluminium composite propellant with low combustion temperature under the condition of spinning burning was investigated.
    启动鱼雷动力系统的固体推进剂药柱系低燃温、无铝复合推进剂,处于旋转状态下燃烧。
短句来源
    The results show that the ST propellant has the characteristics of higher energy,low combustion temperature,low ablation and high overload resistance and can meet the design specification of assorted types of rocket-assisted BB projectile.
    结果表明,ST推进剂具有能量较高(相对总体指标)、低燃温、低烧蚀、抗过载能力强的特点,可以满足不同型号复合增程炮弹火箭增程设计要求。
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The energy characteristics of hydroxylammonium nitrate (HAN)-triethanolammonium nitrate(TEAN)-H_2O liquid mon propellants has been evaluatel. It is found that fuel-rich or oxidizer0richmixtres obtain lower combustion temperature and higher voluminal energy density than thefuel / oxidiger ratio at maxiumn impetes.

本文对HAN-TEAN-H_2O单元液体发射药的能量特性进行了研究.提出采用富燃料或富氧化剂配方.比采用最大火药力的配方得到较低的燃温与较高的体积能量密度。

he Performance of nonaluminium composite propellant with low combustion temperature under the condition of spinning burning was investigated. The propellant is used to drive underwater propulsion system. The results show the effect of acceleration on combustion of nonalumiumcomposite propellant: the chamber pressure will increase and the burning time will decreased with theacceleration.

启动鱼雷动力系统的固体推进剂药柱系低燃温、无铝复合推进剂,处于旋转状态下燃烧。本项研究利用旋转燃烧试验台进行了药柱的燃烧试验,显示了加速度对无铝推进剂燃烧的影响。结果表明:在试验条件范围内,推进剂药柱随着加速度增大,燃烧室压强增大、燃烧时间缩短。根据实验数据整理出旋转燃烧条件下燃速公式。

In order to increase the firing range of composite rocket-assisted projectile and decrease the ablation of nozzle,the ST propellant used for rocket-assisted BB projectile is developed.The Φ50mm motor steel nozzle′s ablation experiment,static and dynamic experiment of an certain rocket-assisted BB projectile moter and intension experiment are carried out.The results show that the ST propellant has the characteristics of higher energy,low combustion temperature,low ablation and high overload resistance and can...

In order to increase the firing range of composite rocket-assisted projectile and decrease the ablation of nozzle,the ST propellant used for rocket-assisted BB projectile is developed.The Φ50mm motor steel nozzle′s ablation experiment,static and dynamic experiment of an certain rocket-assisted BB projectile moter and intension experiment are carried out.The results show that the ST propellant has the characteristics of higher energy,low combustion temperature,low ablation and high overload resistance and can meet the design specification of assorted types of rocket-assisted BB projectile.

为提高复合增程炮弹的射程,降低喷管的烧蚀性,研制了复合增程炮弹用ST推进剂。进行了Φ50mm发动机钢质喷管烧蚀试验、某复合增程炮弹实际发动机的静、动态及强度试验。结果表明,ST推进剂具有能量较高(相对总体指标)、低燃温、低烧蚀、抗过载能力强的特点,可以满足不同型号复合增程炮弹火箭增程设计要求。

 
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