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Hypersonic Airplane Space Tether Orbital Launch (HASTOL) System: Interim Study Results

机译：高超音速飞机太空系绳轨道发射（HasTOL）系统：中期研究结果

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Thomas J. Bogar presenter; Michal E. Bangham; Robert L. Forward; Mark J. Lewis; Dr. Thomas J. Bogar presenter; Senior Principal Engineer; Hypersonic Design;
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1. Analytical study of the performance of electrodynamic tether orbit transfer system with consideration of lifetime by the impact of space debris [J] . Yoshiki Yamagiwa, Yukitaka Sakata, Tatsuya Hashimoto Transactions of the Japan society for aeronautical and space sciences . 2002,第146期

机译：考虑空间碎片影响的寿命的电动系链轨道传输系统性能的分析研究
2. Evolution of space tethered system's orbit during space debris towing taking into account the atmosphere influence [J] . Ledkov Alexander, Aslanov Vladimir Nonlinear dynamics . 2019,第3期

机译：太空碎片牵引过程中空间系圈系统轨道的演变考虑到大气影响
3. Real time control of tethered satellite systems to de-orbit space debris [J] . Razzaghi Pouria, Al Khatib Ehab, Bakhtiari Shide, Aerospace science and technology . 2021,第Feba期

机译：将卧系卫星系统的实时控制到轨道空间碎片
4. Hypersonic Airplane Space Tether Orbital Launch (HASTOL) System: Initial Study Results [C] . Dr.Robert L.Forward, Dr.Thomas J.Bogar, Michal E.Bangham, IAF 50th International Astronautical Congress October 4-8, 1999/Amsterdam, The Netherlands . 1999

机译：高超音速飞机航天栓轨道发射（HASTOL）系统：初步研究结果
5. Computational Pipeline to Find Optimal Launch and Closure Strategy for Autonomous Tether-Net Space Debris Capture System [D] . Shah, Raj Kalpeshkumar. 2021

机译：计算管道为自主系绳净空间碎片捕获系统找到最佳发射和闭合策略
6. Airplanes Crash SpaceshipsStay in Orbit [O] . RITA S. EAGLE 1993

机译：飞机坠毁飞船留在轨道上
7. Benefits and Risks of using Electrodynamic Tethers to De-Orbit Spacecraft - Space Tether Survivability Concerns [O] . Pardini Carmen 2004

机译：使用电动系链带使航天器脱离轨道的好处和风险-系链带生存能力的担忧

Hypersonic Airplane Space Tether Orbital Launch (HASTOL) System: Interim Study Results

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