| 运载火箭的自旋稳定问题 |
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| 引用本文： | 刘绍球
,张道星.运载火箭的自旋稳定问题[J].中国空间科学技术,1986,6(6):59. |
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| 作者姓名： | 刘绍球 张道星 |
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| 摘 要： | 本文讨论卫星运载火箭末级自旋稳定问题,分析了干扰因素的影响。计算结果表明:卫星入轨点轨道参数的偏差,不仅依赖于干扰因素的性质和作用的大小,而且与末级火箭的转速有关;合理地选择末级火箭的自身旋转速度,可以减少干扰因素对入轨点轨道参数偏差的影响。
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SPIN STABILIZATION OF SATELLITE-LAUNCHER UPSTAGE |
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| Liu Shaoqiu Zhang Daoxing.SPIN STABILIZATION OF SATELLITE-LAUNCHER UPSTAGE[J].Chinese Space Science and Technology,1986,6(6):59. |
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| Authors: | Liu Shaoqiu Zhang Daoxing |
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| Abstract: | This papar presents preliminary assessment about spin stabilization of satellite-launcher upstage and analyses the influence of the interference factors. The calculated results indicate that the deviation of satellite insertion point orbit parameters not only depends on the character and the influence degree of the interference factors; and relates to the spin speed of satellite-launcher upstage as well. The correct determination of the spin speed of the launcher upstage can diminish the influence of the interference factors on the insention point orbin parameters. |
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