The Manner of Spacecraft Protection from Potential Impact of Space Debris as the Problem of Selection with Fuzzy Logic

Author:

Paliukh B. V.ORCID,Kemaykin V. K.ORCID,Kozlova Yu. G.ORCID,Kozhukhin I. V.ORCID

Publisher

Springer International Publishing

Reference15 articles.

1. Kobylkin, I.F., Selivanov, V.V.: Materials and Structures of Light Armor Protection. BMSTU, Moscow, Russia (2014). (in Russian)

2. Gerasimov, A.V., Pashkov, S.V., Khristenko, Yu. F.: Protection of spacecraft from anthropogenic and natural fragments. Experiment and numerical simulation [Bull. Tomsk State Univ. Math. Mech.] 4(16), 70–78 (2011). (in Russian)

3. Ryan, S., Christiansen, E.L.: NASA/TM-2009-000000. Honeycomb vs. Foam: Evaluating a Potential Upgrade to ISS Module Shielding for Micrometeoroids and Orbital Debris. NASA, 2009

4. Destefanis, R., Amerio, E., Briccarello, M., Belluco, M., Faraud, M., Tracino, E., Lobascio, C.: Space environment characterisation of Kevlar: good for bullets, debris and radiation too. Univ. J. Aeronaut. Aerosp. Sci. 2, 80–113 (2014)

5. Destefank, D., Lambert, M., Schäfer, F., Drolshagen, G., Francesconi, D.: Debris shielding development for the ATV integrated cargo carrier. In: Proceedings of the 4th European Conference on Space Debris. ESA/ESOC: Darmstadt, Germany, 2005, pp. 453–458. Available at: http://adsabs.harvard.edu/full/2005ESASP.587..453D.html . Accessed 27 July 2018

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