A CLOSED FORM APPROXIMATE SOLUTION FOR THE INITIAL REENTRY ANGLE AND VELOCITY OF OBJECTS DECAYING FROM CIRCULAR ORBITS AROUND AN OBLATE ROTATING PLANET (EVALUATED FOR EARTH FOR SIX ATMOSPHERIC MODELS),

著录项

• 作者

  spahr, h. r.;

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• 作者单位

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• 年度 1968
• 页码 1-240
• 总页数 240
• 原文格式 PDF
• 正文语种 eng
• 中图分类 工业技术;
• 关键词

  atmosphere entry; spacecraft nuclear propulsion; spacecraft nuclear propulsion; safetyatmosphere models; descent trajectories; circular orbit trajectories; solar radiation; mathematical models; approximation(mathematics); gravity; drag; computer programs;

  机译：大气进入;航天器核推进;航天器核推进;安全大气模型;下降轨迹;圆轨道轨迹;太阳辐射;数学模型;近似（数学）;重力;阻力;计算机程序;