Optimum Trajectories for an Earth–Asteroid–Earth Mission with a High Thrust Flight

Author:

Ivashkin V. V.,Lang A.

Publisher

Pleiades Publishing Ltd

Subject

General Physics and Astronomy,Mechanics of Materials,Computational Mechanics

Reference13 articles.

1. Exploration of Cosmic Space by Means of Reaction Devices;K. E. Tsiolkovsky,1964

2. S. A. Sandford, Proc. Int. Astron. Union 7 (S280), 275 (2011).

3. T. Ajluni, D. Everett, T. Linn, et al., OSIRIS-REx, Returning the Asteroid Sample, in 2015 IEEE Aerospace Conference, pp. 1–15.

4. Automatic Spacecrafts for Fundamental and Applied Scientific Investigations, Ed. by G. M. Polishchuk and K. M. Pichkhadze (MAI-PRINT, Moscow, 2010) [in Russian].

5. V. V. Ivashkin and A. Lang, Dokl. Phys. 61, 288 (2016).

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2. Emergency seismic sensing method of asteroid structure;Journal of Physics: Conference Series;2020-05-01

3. Construction of the Optimal Trajectories for the Earth–Asteroid–Earth Mission under High-Thrust Flight;Cosmic Research;2020-03

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