| 战术导弹固体发动机的关键技术问题 |
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| 引用本文： | 阮崇智.战术导弹固体发动机的关键技术问题[J].固体火箭技术,2002,25(2):8-12. |
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| 作者姓名： | 阮崇智 |
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| 作者单位： | 中国航天科技集团公司四院,西安,710025 |
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| 摘 要： | 讨论了战术导弹固体发动机在高能推进剂、碳纤维壳体、轻质小力矩柔性喷管和双脉冲发动机等关键技术方面取得的进展。其中，HTPB推进剂的性能达到比较完善的水平，已用于各类战术导弹。高能、低特征信号GAP推进剂通过了实验发动机试验。碳纤维壳体达到了实用水平。发动机能量管理和向量控制技术的研制与开发工作正在开展之中。
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| 关 键 词： | 战术导弹 固体推进剂 火箭发动机 复合推进剂 喷管 碳纤维壳体 |
| 文章编号： | 1006-2793(2002)02-0008-05 |
Key technical problems for tactical missile solid rocket motors |
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| RUAN Chong-zhiThe Fourth Academy of CASC,Xi'an ,China..Key technical problems for tactical missile solid rocket motors[J].Journal of Solid Rocket Technology,2002,25(2):8-12. |
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| Authors: | RUAN Chong-zhiThe Fourth Academy of CASC Xi'an China |
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| Institution: | RUAN Chong-zhiThe Fourth Academy of CASC,Xi'an 710025,China. |
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| Abstract: | The evolution in some respects of key technical problems such as high energy propellant, carbon-fiber wound case, lightweight low-torque flexible nozzle and double pulse motor etc for tactical missile solid rocket motors are discussed.It is considered that the technical performaces of HTPB propellant has been perfect and widely used for various tactical missiles; the high-energy and low signature GAP propellant has passed the test of test motor; the carbon-fiber wound case has been brought to practical use.And the research and development of motor energy management and thrust vector control (TVC) technique are being carried out. |
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| Keywords: | tactical missile solid propellant rocket engine composite propellant carbon fiber reinforced composite flexible nozzle |
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