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Giuseppe Gallo
Giuseppe Gallo
在 hawaii.edu 的电子邮件经过验证
标题
引用次数
引用次数
年份
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
202021
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
202021
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
202021
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
152023
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
92020
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
82023
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
82019
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
72022
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
52023
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
52023
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
42024
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
42024
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
42021
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
22024
Model for Combustion Instability in Hybrid Rocket Engines Burning Liquefying Fuels
G Gallo, C Carmicino
AIAA Journal 61 (8), 3375-3392, 2023
22023
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
22023
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
22022
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
12024
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
12023
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
12023
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