Using the inertia of spacecraft during landing to penetrate regoliths of the Solar System-Reference-Cited by-同舟云学术

Using the inertia of spacecraft during landing to penetrate regoliths of the Solar System

Published:2015-09 Issue:6 Volume:56 Page:1242-1263
ISSN:0273-1177
Container-title:Advances in Space Research
language:en
Short-container-title:Advances in Space Research

Author:

Paton M.D.,Green S.F.,Ball A.J.,Zarnecki J.C.,Harri A.-M.

Funder

Royal Astronomical Society

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference42 articles.

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4. Ballouz, R., Richardson, D.C., Michel, P., Schwartz, S.R. (2014). Numerical simulations of spacecraft-regolith interactions on asteroids. In: AAS/Division for Planetary Sciences Meeting Abstracts, AAS/Division for Planetary Sciences Meeting Abstracts, vol. 46, p. 213.03.

5. Bolton, M.D., Gui, M.W., 1993. The study of relative density and boundary effects for cone penetration tests in centrifuge, Report CUED/D-SOILS/TR256. Technical Report Cambridge University, Engineering Department, UK.

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