| 引用本文: | 黄卫东,王克昌,陈启智.单级入轨运载器干质量影响因素分析.[J].国防科技大学学报,1997,19(3):89-91.[点击复制] |
| Huang Weidong,Wang Kechang,Chen Qizhi.The Analysis of the Effects of the Dry Mass of Single-Stage-to-Orbit Vehicle[J].Journal of National University of Defense Technology,1997,19(3):89-91[点击复制] |
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| 单级入轨运载器干质量影响因素分析 |
| 黄卫东, 王克昌, 陈启智 |
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(国防科技大学 航天技术系 湖南 长沙 410073)
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| 摘要: |
| 提出了单级入轨运载器干质量计算方法。对给定的飞行任务, 提出了基准运载器, 并计算了贮箱材料、热防护系统及设计余量对运载器干质量的影响。计算结果表明, 先进的材料和设计能降低运载器的干质量, 并使运载器干质量对设计余量的敏感性降低。 |
| 关键词: 单级入轨, 运载器干质量, 设计余量 |
| DOI： |
| 投稿日期：1996-07-01 |
| 基金项目: |
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| The Analysis of the Effects of the Dry Mass of Single-Stage-to-Orbit Vehicle |
| Huang Weidong, Wang Kechang, Chen Qizhi |
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(Department of Astronautic Technology, NUDT, Changsha, 410073)
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| Abstract: |
| A method to calculate the dry mass of single-stage vehicle is proposed in this paper. A baseline vehicle is presented for the given flight mission, and the effects of the tank material, the thermal protection system and the design margin on the vehicle dry mass are calculated. The calculation results show that the advanced material and design can decrease the vehicle dry mass and its sensitivity to the design margin. |
| Keywords: single stage to orbit, vehicle dry mass, design margin |
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