Tether-assisted re-entry capsule deorbiting from an elliptical orbit

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• 作者：Vladimir S. Aslanov ; ^{aslanov_vs@mail.ru} ; ; Alexander S. Ledkov ^{ledkov@inbox.ru}
• 关键词：Space tether ; Re-entry ; Deorbiting ; Elliptic orbit ; Thermal loads
• 刊名：Acta Astronautica
• 出版年：2017
• 出版时间：January-February 2017
• 年：2017
• 卷：130
• 期：Complete
• 页码：180-186
• 全文大小：1251 K
• 卷排序：130

文摘

The radius of perigee cannot be a single indicator of tether deployment efficiency. Separation points that provide minimum thermal and mechanical constrains were found. Separation at the local vertical does not guarantee the minimum radius of perigee.