| 1. | Hypergolic ignition systems bear many resemblances to hybrid rockets .
自然式点火系统在很多方面与混合型火箭相似。 |
| 2. | Model about regression rate of hybrid rocket motors was studied
研究了固液发动机固体燃料退移速率预示模型。 |
| 3. | The low frequency burning oscillation of the 85 % h202 - pe hybrid rocket motor is discussed
研究了85 hzoz ? pe固液火箭发动机的低频振荡燃烧现象。 |
| 4. | The combustion model of hybrid rocket propellant was established . the combustion flow in the hno3 + n2o4 - htpb hybrid rocket motor has been researched
研究了直径为706mm多孔分段装药全尺寸试验固液火箭发动机内部的燃烧与流动问题。 |
| 5. | The catalytic decomposition of 85 % hydrogen peroxide , the pyrolysis of the polyethylene fuel and the energy performance of the h2o2 - pe hybrid rocket motor were all discussed
研究了85过氧化氢氧化剂的催化分解性能、 pe燃料的热解性能以及过氧化氢和pe燃料组合的能量特性。 |
| 6. | Through the tests of the 85 % h2o2 - pe hybrid rocket motor , the operation process of the hybrid motor has been studied in the dissertation . the main aspects are as follows : 1
本文结合85 h _ 2o _ 2 ? pe固液火箭发动机试验，从以下几个方面比较系统地研究了固液火箭发动机的工作过程： 1 |
| 7. | 5 . the internal ballistics and the throttling performance of 85 % h2o2 - pe hybrid rocket motor loaded with tube grain are studied . the hot firing data of two test motors have been carefully analyzed
研究了管型药柱的85 h _ 2o _ 2 - pe固液火箭发动机的内弹道性能和节流特性，分析了两台发动机的试验结果。 |
| 8. | The pressurized 85 % h2o2 - pe hybrid rocket motor test system has been designed and built up for the research work . the hot firing tests and the shutdown - restart of the motor were successfully performed . 2
设计和建造了85 h _ 2o _ 2 ? pe固液火箭试验发动机和挤压式固液火箭发动机试验系统，并成功地进行了点火和再启动。 |
| 9. | Because of their low - cost , high safety and reliability , flexible energy management and shutdown - restart ability , hybrid rocket motors have received increasing attention from the space propulsion specialist all over the world
固液火箭发动机因具有低成本、高安全性和可靠性、灵活的能量管理和推力可控等特性,越来越受到国内外航天推进专家的重视。 |
| 10. | Because of their low - cost , high safety and reliability , flexible energy management and shutdown - restart ability , hybrid rocket motors have received increasing attention from the space propulsion specialist all over the world
固液火箭发动机因具有低成本、高安全性和可靠性、灵活的能量管理和多次启动等优良特性，越来越受到国内外航天推进专家的重视。 |
