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Review of ballistic limit equations for cfrp structure walls of satellites
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Schäfer F, Schneider E, Lambert M (2004). Review of Ballistic Limit Equations for CFRP Structure Walls of Satellites. Proceedings of the 5th International Symposium on Environmental Testing for Space Programs, ESA SP-558, Noordwijk, The Netherlands.
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Hypervelocity impact testing of cfrp/al honeycomb satellite structures
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Numerical simulation of hypervelocity impact on cfrp/al hc/sp spacecraft structures causing penetration and fragment ejection
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Ryan S, Schäfer F, Riedel W (2006). Numerical Simulation of Hypervelocity Impact on CFRP/Al HC/SP Spacecraft Structures Causing Penetration and Fragment Ejection. International Journal of Impact Engineering, 33:703-712.
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Vulnerability of shielded fuel pipes and heat pipes to hypervelocity impacts
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Putzar R, Schäfer F, et al (2005). Vulnerability of Spacecraft Electronic Boxes to Hypervelocity Impacts. Paper No. IAC-05-B.6.4.02, Proceedings of the 56th International Astronautical Congress, Fukuoka, Japan.
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Ballistic limit equation for equipment placed behind satellite structure walls
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Ryan S, Schäfer F, et al (2007). A Ballistic Limit Equation for Hypervelocity Impacts on Composite Honeycomb Sandwich Panel Satellite Structures. Advances in Space Research, 41(7):1152-1166.
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Schonberg WP, Schäfer F, Putzar R (2009). Effectiveness of HC/SP Ballistic Limit Equations in Predicting Perforation /Non-Perforation Response. Journal of Spacecraft and Rockets, submitted for publication consideration.
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Ryan, S (2009). Numerical Simulation in Micrometeoroid and Orbital Debris Risk Assessment. In Predictive Modeling of Dynamic Processes: A Tribute to Klaus Thoma, ed. S. Hiermaier, Springer, Berlin Germany.
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Acta Astronautica
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