| 平飞固体火箭助推器设计 |
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| 引用本文： | 陈光学,白彦军,王铮.平飞固体火箭助推器设计[J].固体火箭技术,2003,26(4):6-8,78. |
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| 作者姓名： | 陈光学 白彦军 王铮 |
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| 作者单位： | 1. 西北工业大学航天学院,西安,710072
2. 中国航天科技集团公司中天火箭技术有限责任公司,西安,710025 |
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| 摘 要： | 介绍平飞固体火箭助推器的设计，重点是固体助推器主要参数的确定和助推器壳体的传热分析，给出具体算例，并与试验进行比较，结果表明设计是正确的。
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| 关 键 词： | 平飞固体火箭 助推器 设计 传热分析 总换热系数 固体推进剂火箭 |
| 文章编号： | 1006-2793(2003)04-0006-03 |
The booster design on flat flight solid rocket |
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| CHEN Guang-xue,BAI Yan-jun,WANG Zheng//. Coll. of Astronautics,Northwestern Polytechnical University,Xi'an,China, . Zhongtian Rocket Technology Limited-liability Company of CSAC,Xi'an,China..The booster design on flat flight solid rocket[J].Journal of Solid Rocket Technology,2003,26(4):6-8,78. |
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| Authors: | CHEN Guang-xue BAI Yan-jun WANG Zheng// Coll of Astronautics Northwestern Polytechnical University Xi'an China Zhongtian Rocket Technology Limited-liability Company of CSAC Xi'an China |
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| Institution: | CHEN Guang-xue~1,BAI Yan-jun~2,WANG Zheng~2//1. Coll. of Astronautics,Northwestern Polytechnical University,Xi'an710072,China, 2. Zhongtian Rocket Technology Limited-liability Company of CSAC,Xi'an710025,China. |
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| Abstract: | The booster of a flat flight solid rocket is introduced. The focal points of introduction are to establish the main parameters of the solid rocket booster and the heat transfer analysis of the booster case. The practical example is given and its design parameters are compared with its tested results. It is indicated that the design and analysis methods are correct. |
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| Keywords: | solid propellant rocket sustainer rocket engine booster |
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