Numerical Simulation in Micrometeoroid and Orbital Debris Risk Assessment

Author:

Ryan Shannon

Publisher

Springer US

Reference28 articles.

1. Jones, J.: Meteoroid Engineering Model ’ Final Report. University of Western Ontario, London, NASA SEE/CR-2004-400 (2004)

2. Liou, J-C., Matney, M., Anz-Meador, P., Kessler, D., Jansen, M., Theall, J.: The New NASA Orbital Debris Engineering Model ORDEM2000. Lockheed Martin Space Operations, Houston, NASA TP-2002-210780 (2002)

3. Cour-Palais, B.: Hypervelocity Impact Investigations and Meteoroid Shielding Experience Related to Apollo and Skylab. Orbital Debris, 247–275 (1982)

4. Christiansen E., Kerr, J.: Ballistic Limit Equations for Spacecraft Shielding. International Journal of Impact Engineering 26, 93–104 (2001)

5. Christiansen, E., Kerr, J.: Ballistic Limit Equations for Spacecraft Shielding. International Journal of Impact Engineering 26, 93-104 (2001)

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