AEROSPACE SHANGHAI, Volume. 41, Issue 6, 55(2024)
Application of 3D Geographic Information System in Situation Decision on Rocket Safety Control and Its Key Techniques
Figures & Tables(7)
Fig. 1. Architecture diagram of the management and application system for 3D safety control geographic information
Fig. 3. The definition and transformation method of the predicted landing point coordinate system
Table 1.
Parameters of some medium launch vehicles in China View tableView in ArticleTable 1.
Parameters of some medium launch vehicles in China 型号 总长/m 起飞质量/t 火箭构型 火箭燃料 长征二号F 58.34 493 常温液体运载火箭 四氧化二氮+偏二甲肼 长征四号乙 45.576 249.2 常温液体运载火箭 四氧化二氮+偏二甲肼 长征四号丙 47.977 250 常温液体运载火箭 四氧化二氮+偏二甲肼 长征五号 56.97 869 低温液体捆绑运载火箭 液氢液氧、液氧煤油 长征五号乙 53.7 837.5 低温液体捆绑运载火箭 液氢液氧、液氧煤油 长征六号甲 50 530 固液捆绑运载火箭 液氧煤油、固体高能燃料
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Zhijian YU, Jiuwen YANG, Pengchong GU, Zhenlong YUAN. Application of 3D Geographic Information System in Situation Decision on Rocket Safety Control and Its Key Techniques[J]. AEROSPACE SHANGHAI, 2024, 41(6): 55
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Category: Innovation and Exploration
Received: Aug. 28, 2024
Accepted: --
Published Online: Mar. 7, 2025
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