| 引用本文: | 甘楚雄.织女一号气象火箭设计中的若干技术.[J].国防科技大学学报,1989,11(3):16-25.[点击复制] |
| Gan Chuxiong.Some Technology in Design of the ZN-l Meteorological Rocket[J].Journal of National University of Defense Technology,1989,11(3):16-25[点击复制] |
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| 织女一号气象火箭设计中的若干技术 |
| 甘楚雄 |
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(航天技术系)
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| 摘要: |
| 织女一号气象火箭是一种小型无控固体火箭，由于采用了若干先进的技术，使其总体性能达到了国际先进水平。本文介绍了其总体性能，重点介绍了总体方案设计中采用的包括最优推力程序等若干先进技术。 |
| 关键词: 气象火箭，固体火箭，最优推力程序，端面燃烧装药 |
| DOI： |
| 投稿日期：1988-08-30 |
| 基金项目: |
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| Some Technology in Design of the ZN-l Meteorological Rocket |
| Gan Chuxiong |
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(Department of Aerospace Technology)
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| Abstract: |
| The ZN-l Meteorological Rocket is designed in need of development of space technology. The overall performances of rocket have reached the advanced world level by means of using some advanced technology. This paper centers on some advanced technology adopted in the overall design，such as optimal thrust program. |
| Keywords: Moteorological rocket,solid rocket,optimal thrust program,a end buring grain |
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