| Engine for hypersonic aircrafts with supersonic combustor M Gabaldo, JEM BARROS US Patent 10,927,793, 2021 | 7 | 2021 |
| Aerothermodynamic simulation model for new hypersonic propulsion: Rocket ignited supersonic combustion ram jet M Gabaldo, JE Barros, MD Guerra, E Oliveira AIAA SPACE 2016, 5323, 2016 | 5 | 2016 |
| Aerothermodynamics cycle model for new hypersonic propulsion: Rocket Ignited Supersonic Combustion Ram Jet JE Barros, M Gabaldo, MD Guerra 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 4872, 2016 | 3 | 2016 |
| Technical and Economic Feasibility Analysis of a Two Stage Reusable Satellite Launcher Using RISCRAM™ Jet Engines M Gabaldo, OR Barros, JEM Barros SAE Technical Paper, 2017 | 2 | 2017 |
| Wind Tunnel Balance LBS Alves, M Gabaldo, LS Dutra, JEM Barros SAE Technical Paper, 2017 | 1 | 2017 |
| RISCRAM™: propulsore ipersonico M Gabaldo http://www.aviation-report.com/riscram-propulsore-ipersonico/, 2017 | | 2017 |
| Engine for hypersonic aircrafts with supersonic combustor G Marco, JE MAUTONE BARROS WO Patent 2016157224 A1, 2016 | | 2016 |
| CFD Study of Reactive Compressible Systems P Bianca Teixeira and Raphael Bacci, ESSS / José Barros, UFMG / Marcelo ... ESC | Energy Simulation Conference - CFD OIL 2016, 2016 | | 2016 |
