Combining magnetic and electric sails for interstellar deceleration

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• 作者：Nikolaos Perakis^a ; ^{nikolaos.perakis@tum.de" class="auth_mail" title="E-mail the corresponding author} ; Andreas M. Hein^b ; ^{andreas.hein@i4is.org" class="auth_mail" title="E-mail the corresponding author}
• 关键词：Magnetic sail ; Electric sail ; Interstellar mission ; Mission design ; Optimization
• 刊名：Acta Astronautica
• 出版年：2016
• 出版时间：November-December 2016
• 年：2016
• 卷：128
• 期：Complete
• 页码：13-20
• 全文大小：765 K

文摘

The main benefit of an interstellar mission is to carry out in situ measurements within a target star system. To allow for extended in situ measurements, the spacecraft needs to be decelerated. One of the currently most promising technologies for deceleration is the magnetic sail which uses the deflection of interstellar matter via a magnetic field to decelerate the spacecraft. However, while the magnetic sail is very efficient at high velocities, its performance decreases with lower speeds. This leads to deceleration durations of several decades depending on the spacecraft mass. Within the context of Project Dragonfly, initiated by the Initiative of Interstellar Studies (i4is), this paper proposes a novel concept for decelerating a spacecraft on an interstellar mission by combining a magnetic sail with an electric sail. Combining the sails compensates for each technology's shortcomings: a magnetic sail is more effective at higher velocities than the electric sail, whereas an electric sail demonstrates superior performance at low speeds. It is shown that using both sails sequentially outperforms using only the magnetic or electric sail for various mission scenarios and velocity ranges, at a constant total spacecraft mass. For example, for decelerating from 5% c, to interplanetary velocities, a spacecraft with both sails needs about 29 years, whereas the electric sail alone would take 35 years and the magnetic sail about 40 years with a total spacecraft mass of 8250 kg. Furthermore, it is assessed how the combined deceleration system affects the optimal overall mission architecture for different spacecraft masses and cruising speeds. Future work would investigate how operating both systems in parallel instead of sequentially would affect its performance. Moreover, uncertainties in the density of interstellar matter and sail properties need to be explored.