| Handbook for Designing MMOD Protection EL Christiansen, J Arnold, B Corsaro, A Davis, F Giovane, J Hyde, D Lear, ... NASA Johnson Space Center, NASA/TM-2009-214785, 2009 | 173 | 2009 |
| The effect of target thickness on the ballistic performance of ultra high molecular weight polyethylene composite LH Nguyen, S Ryan, SJ Cimpoeru, AP Mouritz, AC Orifici International Journal of Impact Engineering 75, 174-183, 2015 | 161 | 2015 |
| Hypervelocity impact on CFRP: Testing, material modelling, and numerical simulation M Wicklein, S Ryan, DM White, RA Clegg International Journal of Impact Engineering 35 (12), 1861-1869, 2008 | 133 | 2008 |
| A ballistic limit equation for hypervelocity impacts on composite honeycomb sandwich panel satellite structures S Ryan, F Schaefer, R Destefanis, M Lambert Advances in Space Research 41 (7), 1152-1166, 2008 | 125 | 2008 |
| A methodology for hydrocode analysis of ultra-high molecular weight polyethylene composite under ballistic impact LH Nguyen, TR Lässig, S Ryan, W Riedel, AP Mouritz, AC Orifici Composites Part A: Applied Science and Manufacturing 84, 224-235, 2016 | 122 | 2016 |
| Hypervelocity impact testing of advanced materials and structures for micrometeoroid and orbital debris shielding S Ryan, EL Christiansen Acta Astronautica 83, 216-231, 2013 | 85 | 2013 |
| Honeycomb vs. foam: Evaluating potential upgrades to ISS module shielding S Ryan, T Hedman, EL Christiansen Acta Astronautica 67 (7-8), 818-825, 2010 | 74 | 2010 |
| Theoretical prediction of dynamic composite material properties for hypervelocity impact simulations S Ryan, M Wicklein, A Mouritz, W Riedel, F Schäfer, K Thoma International Journal of Impact Engineering 36 (7), 899-912, 2009 | 67 | 2009 |
| The ballistic performance of an ultra-high hardness armour steel: An experimental investigation S Ryan, H Li, M Edgerton, D Gallardy, SJ Cimpoeru International journal of impact engineering 94, 60-73, 2016 | 66 | 2016 |
| Micrometeoroid and orbital debris (MMOD) shield ballistic limit analysis program S Ryan, EL Christiansen Johnson Space Center, 2010 | 61 | 2010 |
| Numerical simulation of hypervelocity impact on CFRP/Al HC SP spacecraft structures causing penetration and fragment ejection S Ryan, F Schaefer, W Riedel International journal of impact engineering 33 (1-12), 703-712, 2006 | 60 | 2006 |
| Ballistic limit equation for equipment placed behind satellite structure walls FK Schäfer, S Ryan, M Lambert, R Putzar International Journal of Impact Engineering 35 (12), 1784-1791, 2008 | 52 | 2008 |
| Numerical modelling of ultra-high molecular weight polyethylene composite under impact loading LH Nguyen, TR Lässig, S Ryan, W Riedel, AP Mouritz, AC Orifici Procedia Engineering 103, 436-443, 2015 | 47 | 2015 |
| Hypervelocity Impact Performance of Open Cell Foam Core Sandwich Panel Structures S Ryan, E Ordonez, EL Christiansen, DM Lear Proc. 11th Hypervlocity Impact Symposium, 2010 | 38 | 2010 |
| The efficiency of ultra-high molecular weight polyethylene composite against fragment impact LH Nguyen, S Ryan, SJ Cimpoeru, AP Mouritz, AC Orifici Experimental Mechanics 56, 595-605, 2016 | 37 | 2016 |
| Machine learning methods for predicting the outcome of hypervelocity impact events S Ryan, S Thaler, S Kandanaarachchi Expert Systems with Applications 45, 23-39, 2016 | 37 | 2016 |
| A ballistic limit analysis programme for shielding against micrometeoroids and orbital debris S Ryan, EL Christiansen Acta Astronautica 69 (5-6), 245-257, 2011 | 36 | 2011 |
| Whipple shield performance in the shatter regime S Ryan, M Bjorkman, EL Christiansen International Journal of Impact Engineering 38 (6), 504-510, 2011 | 35 | 2011 |
| Characterizing the transient response of CFRP/Al HC spacecraft structures induced by space debris impact at hypervelocity S Ryan, F Schäfer, M Guyot, S Hiermaier, M Lambert International Journal of Impact Engineering 35 (12), 1756-1763, 2008 | 31 | 2008 |
| Physical mechanisms for near-field blast mitigation with fluid containers: Effect of container geometry H Bornstein, S Ryan, A Mouritz International journal of impact engineering 96, 61-77, 2016 | 29 | 2016 |
