A Method for Express Analysis of Mechanical, Erosion, and Contaminating Impact of Plasma Jet of Electric Propulsion Thruster onto the Large Object of Space Debris

Author:

Blyakharskii S. S.,Blyakharskii Ya. S.,Nadiradze A. B.,Rakhmatullin R. R.

Publisher

Allerton Press

Subject

Aerospace Engineering

Reference14 articles.

1. Kitamura, S., Large Space Debris Reorbiter Using Ion Beam Irradiation, Proc. 61st Int. Astronautical Congress, Prague, 2010, Paper IAC-10-A6.4.8, pp. 5668–5674.

2. Aslanov, V.S. and Yudintsev, V.V., Docking with Space Debris Employing the Unfolding Flexible Beam-Strap, Vestnik MAI, 2018, vol. 25, no. 2, pp. 16–24.

3. Yudintsev, V.V., Rotating Space Debris Object Net Capture Dynamic, Vestnik MAI, 2018, vol. 25, no. 4, pp. 37–48.

4. Bombardelli, C. and Pelaez, J., Ion Beam Shepherd for Asteroid Deflection, J. of Guidance, Control and Dynamics, 2011, vol. 34, no. 4, pp. 1270–1272.

5. Kim, V.P., Nadiradze, A.B., Popov, G.A., Khodnenko, V.P., and Shishkin, G.G., Problems of Applying Electric Propulsion Thrusters in Spacecraft, in Model’ kosmosa (Space Model), Novikov, L.S., Ed., Moscow: Knizhnyi dom Universitet, 2007, vol. 2, Ambient Impact onto Spacecraft Materials and Equipment, pp. 615–659.

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