| 火箭滑轨段弹道研究(之一) |
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| 引用本文： | 徐明友 徐直军. 火箭滑轨段弹道研究(之一)[J]. 弹道学报, 1994, 0(4): 34-39 |
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| 作者姓名： | 徐明友 徐直军 |
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| 作者单位： | 南京理工大学弹道研究所 |
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| 摘 要： | 将火箭发射系统作为研究对象，火箭在发射过程中的运动将是全系统运动的一部分，且体现车体、回转及起落部分对火箭运动的影响，对所建立的综合性弹道模型，开发出了系统软件，并在国内首次计算出４０管１２２毫米火箭起始扰动，其量级与试验结果一致．
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| 关 键 词： | 火箭弹 滑轨段 起始扰动 弹道 研究 |
BALLISTIC RESEARCH ON ROCKET LAUNCHING PHASE |
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| Xu Mingyou,Xu Zhijun. BALLISTIC RESEARCH ON ROCKET LAUNCHING PHASE[J]. Journal of Ballistics, 1994, 0(4): 34-39 |
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| Authors: | Xu Mingyou Xu Zhijun |
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| Abstract: | The rocket launching system is studied in this paper.As rocket motion during launching is considered as one part of the whloe system motions,the influence of vehicle,rotating frame and elevating assembly on rocket motion is embodied in it.The system program of the ballistics model has been develeped and the computed value of the initial disturbances for 40 tubes 122 mm rocket is identical with the test. |
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| Keywords: | ballistics of rocket launching phase initial disturbance |
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