| Formation and Characterization of Nano‐sized RDX Particles Produced Using the RESS‐AS Process JT Essel, AC Cortopassi, KK Kuo, CG Leh, JH Adair Propellants, Explosives, Pyrotechnics 37 (6), 699-706, 2012 | 46 | 2012 |
| Assessment of the performance of ablative insulators under realistic solid rocket motor operating conditions HT Martin, AC Cortopassi, KK Kuo International Journal of Energetic Materials and Chemical Propulsion 16 (1), 2017 | 37 | 2017 |
| Comparison of nozzle throat erosion behavior in a solid-propellant rocket motor and a simulator B Evans, K Kuo, E Boyd, A Cortopassi 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 5421, 2009 | 24 | 2009 |
| Update: a subscale solid rocket motor for characterization of submerged nozzle erosion A Cortopassi, E Boyer, K Kuo 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 5172, 2009 | 16 | 2009 |
| Design and testing of an additively manufactured advanced hybrid rocket motor propulsion unit for CubeSats (PUC) BR McKnight, JE Boyer, PK Nardozzo, A Cortopassi 51st AIAA/SAE/ASEE Joint Propulsion Conference, 4036, 2015 | 15 | 2015 |
| Design of a solid rocket motor for characterization of submerged nozzle erosion A Cortopassi, E Boyer, R Acharya, K Kuo 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 4889, 2008 | 15 | 2008 |
| Synthesis of nano-sized rdx using an ultra-high-pressure RESS system AC Cortopassi, PJ Ferrara, TM Wawiernia, JT Essel International Journal of Energetic Materials and Chemical Propulsion 7 (1), 2008 | 13 | 2008 |
| Hypergolic ignition testing of solid fuel additives with MON-3 oxidizer A Cortopassi, JE Boyer 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 5050, 2017 | 11 | 2017 |
| Erosion of carbon-cloth phenolic nozzles in rocket motors with aluminized solid propellant AC Cortopassi The Pennsylvania State University, 2012 | 11 | 2012 |
| Characterization of nozzle erosion behavior under rocket motor operating conditions B Evans, KK Kuo, AC Cortopassi International Journal of Energetic Materials and Chemical Propulsion 9 (6), 2010 | 11 | 2010 |
| A novel radiative heat flux Measurement technique for Combustion products flowing in Solid rocket motors HT Martin, RW Houim, PJ Ferrara, MJ Degges, AC Cortopassi, JE Boyer, ... International Journal of Energetic Materials and Chemical Propulsion 12 (3), 2013 | 8 | 2013 |
| Characterization and detailed analysis of regression behavior for HTPB solid fuels containing high aluminum loadings TP Kibbey, A Cortopassi, JE Boyer 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 4735, 2017 | 4 | 2017 |
| Real-Time X-ray Radiography Diagnostics of Components in Solid Rocket Motors AC Cortopassi, HT Martin, E Boyer, KK Kuo 9-ISICP Symposium, 2012 | 4 | 2012 |
| Synthesis of Energetic Materials by Rapid Expansion of a Supercritical Solution into Aqueous Solution (RESS-AS) Process JT Essel, AC Cortopassi, KK Kuo, JH Adair, CG Leh, TM Klapoetke DTIC Document, 2010 | 4 | 2010 |
| Synthesis and characterization of coated energetic materials using a RESS-N system JT Essel, AC Cortopassi, KK Kuo International Journal of Energetic Materials and Chemical Propulsion 9 (2), 2010 | 4 | 2010 |
| Effects of high-pressure RESS operating conditions on the size of synthesized nano-scale RDX particles TM Wawiernia, KK Kuo, PJ Ferrara, AC Cortopassi, JT Essel 2008 SAMPE Fall Technical Conference and Exhibition-Multifunctional …, 2008 | 1 | 2008 |
| Development of a ultra-high-pressure RESS system for synthesizing nano-sized energetic materials AC Cortopassi, KK Kuo, PJ Ferrara, TM Wawiernia, JT Essel 2008 SAMPE Fall Technical Conference and Exhibition-Multifunctional …, 2008 | 1 | 2008 |
| Transient plasma enhanced combustion of solid rocket propellants C Medchill, AA Perezselsky, A Cortopassi, AL Briseno, C Brophy, ... Aerospace Science and Technology 148, 109107, 2024 | | 2024 |
| Coaxial rocket injector mixing and combustion via mid-infrared laser absorption tomography AR Keller, RM Spearrin, FA Bendana, D Kaialau, A Perezselsky, ... AIAA SCITECH 2024 Forum, 2420, 2024 | | 2024 |
| High density hybrid rocket motor AJ Sherman, B Werry, A Cortopassi, E Boyer US Patent 11,787,752, 2023 | | 2023 |
