| New entrainment model for modelling the regression rate in hybrid rocket engines G Gallo, S Mungiguerra, R Savino Journal of Propulsion and Power 37 (6), 893-909, 2021 | 20 | 2021 |
| Self-consistent surface-temperature boundary condition for liquefying-fuel-based hybrid rockets internal-ballistics simulation C Carmicino, G Gallo, R Savino International Journal of Heat and Mass Transfer 169, 120928, 2021 | 20 | 2021 |
| Design and testing of a monopropellant thruster based on N2O decomposition in Pd/Al2O3 pellets catalytic bed GD Di Martino, G Gallo, S Mungiguerra, G Festa, R Savino Acta Astronautica 180, 460-469, 2021 | 20 | 2021 |
| Preliminary design and study of 5N HTP monopropellant thruster for small satellites S Cassese, G Gallo, S Mungiguerra, A Cecere, R Savino Acta Astronautica 202, 94-103, 2023 | 15 | 2023 |
| Experimental Investigation of Decomposition with Cylindrical Pellets Catalyst G Gallo, GD Di Martino, G Festa, R Savino Journal of Spacecraft and Rockets 57 (4), 720-727, 2020 | 9 | 2020 |
| One-dimensional modelling of the nozzle cooling with cryogenic oxygen flowing through helical channels in a hybrid rocket G Gallo, L Kamps, S Hirai, C Carmicino, H Nagata Acta Astronautica 210, 176-196, 2023 | 8 | 2023 |
| Recent advancements in experimental and numerical characterization of paraffin-based fuels for hybrid rocket application GD Di Martino, G Gallo, S Mungiguerra, C Carmicino, R Savino, ... AIAA Propulsion and Energy 2019 Forum, 4195, 2019 | 8 | 2019 |
| Regression rate model assessed by ballistic reconstruction technique in hybrid rocket engines burning liquefying fuels G Gallo, R Savino Aerospace Science and Technology 127, 107712, 2022 | 7 | 2022 |
| Compositionally complex catalytic oxide beds free of noble metals for H2O2 fuelled monopropellant thrusters S Cassese, F Monteverde, G Gallo, S Mungiguerra, A Cecere, F Saraga, ... Journal of the European Ceramic Society 43 (11), 4854-4864, 2023 | 5 | 2023 |
| Experimental firing test campaign and nozzle heat transfer reconstruction in a 200 N hybrid rocket engine with different paraffin-based fuel grain lengths D Cardillo, F Battista, G Gallo, S Mungiguerra, R Savino Aerospace 10 (6), 546, 2023 | 5 | 2023 |
| Experimental investigation of regenerative cooling performance in hybrid rocket engines G Gallo, H Kojima, L Kamps, H Nagata Thermal Science and Engineering Progress 49, 102481, 2024 | 4 | 2024 |
| Prediction of the fuel regression-rate in a HDPE single port hybrid rocket fed by liquid nitrous oxide G Gallo, L Kamps, S Hirai, C Carmicino, N Harunori Combustion and Flame 259, 113160, 2024 | 4 | 2024 |
| Numerical aspects of particle-in-cell simulations for plasma-motion modeling of electric thrusters G Gallo, A Isoldi, D Del Gatto, R Savino, A Capozzoli, C Curcio, A Liseno Aerospace 8 (5), 138, 2021 | 4 | 2021 |
| Effect of grain length on GOx-paraffin hybrid rocket engines performance and regression rate G Gallo, S Mungiguerra, R Savino, D Cardillo, F Battista International Journal of Heat and Mass Transfer 220, 124978, 2024 | 2 | 2024 |
| Model for Combustion Instability in Hybrid Rocket Engines Burning Liquefying Fuels G Gallo, C Carmicino AIAA Journal 61 (8), 3375-3392, 2023 | 2 | 2023 |
| Regenerative Cooling of Graphite Nozzles for Throat Erosion Suppression H Kojima, LT Kamps, Y Nobuhara, G Gallo, H Nagata AIAA SCITECH 2023 Forum, 1830, 2023 | 2 | 2023 |
| Experimental characterization of a hydrogen peroxide-based thruster for small satellites S Cassese, G Gallo, S Mungiguerra, A Cecere, C Gobbi, R Savino, ... Proceedings of IAC 2022, 2022 | 2 | 2022 |
| Regenerative cooling in hybrid rocket engines based on Self-Pressurized liquid nitrous oxide G Gallo, Y Miyahara, L Kamps, H Nagata Applied Thermal Engineering 254, 123928, 2024 | 1 | 2024 |
| Experimental Firing Test Campaign and Nozzle Heat Transfer Reconstruction in a 200 N Hybrid Rocket Engine with Different Paraffin-Based Fuel Grain Lengths. Aerosp. 2023, 10, 546 D Cardillo, F Battista, G Gallo, S Mungiguerra, R Savino | 1 | 2023 |
| Numerical Model for the Prediction of the Regression Rate in Hybrid Rocket Kick-Motors Working with Nitrous Oxide G Gallo, LT Kamps, S Hirai, C Carmicino, H Nagata AIAA SCITECH 2023 Forum, 2348, 2023 | 1 | 2023 |
