Micro-meteoroids and space debris impact risk assessment for the ConeXpress satellite using ESABASE2/Debris-Reference-Cited by-同舟云学术

Micro-meteoroids and space debris impact risk assessment for the ConeXpress satellite using ESABASE2/Debris

Published:2010-03 Issue:5 Volume:45 Page:683-689
ISSN:0273-1177
Container-title:Advances in Space Research
language:en
Short-container-title:Advances in Space Research

Author:

Kuiper W.,Drolshagen G.,Noomen R.

Publisher

Elsevier BV

Subject

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

Reference15 articles.

1. Anonymous. Satellite Collision Leaves Significant Debris Clouds, Orbital Debris Quarterly News, vol. 13, issue 2, April 2009.

2. Design and performance equations for advanced meteoroid and debris shields;Christiansen;International Journal of Impact Engineering,1993

3. Cour-Palais, B.C. Space Vehicle Meteoroid Shielding Design. In: Proceedings of ESA workshop 18–19 April 1979, ESTEC, The Netherlands, ESA SP-153, 1979.

4. ECSS, European Cooperation for Space Standardization. Space Engineering, Space Environment, ECSS-E-ST-10-04C, 15 Nov. 2008.

5. eta_max Space. ESABASE2/Debris, Technical Description, Ref. r040_rep025_02_00_01, Release 1.2, Braunschweig, Germany, 2006.

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