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Marco Rotondi
Marco Rotondi
Research Propulsion Engineer, Letara Ltd., Sapporo, Japan
Verifisert e-postadresse på letara.space
Tittel
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Numerical analysis of nozzle erosion in hybrid rockets and comparison with experiments
D Bianchi, MT Migliorino, M Rotondi, L Kamps, H Nagata
Journal of Propulsion and Power 38 (3), 389-409, 2022
212022
Numerical analysis and wind tunnel validation of low-temperature ablators undergoing shape change
D Bianchi, MT Migliorino, M Rotondi, A Turchi
International Journal of Heat and Mass Transfer 177, 121430, 2021
202021
Computational analysis and regression laws for nozzle erosion prediction in hybrid rockets
M Rotondi, MT Migliorino, D Bianchi, L Kamps, H Nagata
Journal of Propulsion and Power 40 (3), 439-459, 2024
62024
Numerical assessment of camphor ablation flight relevance in hypersonic wind-tunnel testing
M Rotondi, MT Migliorino, D Bianchi, P Pagani, A Turchi
Journal of Spacecraft and Rockets 59 (5), 1574-1591, 2022
62022
Numerical analysis of nozzle heating and erosion in hybrid rockets and comparison with experiments
D Bianchi, MT Migliorino, M Rotondi, LT Kamps, H Nagata
AIAA Propulsion and Energy 2020 Forum, 3767, 2020
62020
Student firing tests and launches with commercial and self-made solid rocket motors
MT Migliorino, M Aiello, M Berti, M Rotondi, S D’Alessandro, D Bianchi, ...
Acta Astronautica 197, 23-34, 2022
52022
Development and validation of nozzle erosion models for solid and hybrid rockets in the ESPSS libraries
M Rotondi, P Concio, S D’Alessandro, FR Lucas, D Bianchi, F Nasuti, ...
Proceedings of the Conference: 8th Space Propulsion, Estoril, Portugal, 9-13, 2022
52022
Numerical analysis of nozzle transient heating and erosion in hybrid rockets burning HDPE
M Rotondi, MT Migliorino, D Bianchi, LT Kamps, H Nagata
AIAA Propulsion and Energy 2021 Forum, 3496, 2021
42021
Numerical Analysis of Carbon-based Nozzle Erosion including Transient Heating and Shape Change
M Rotondi, MT Migliorino, D Bianchi
Aiaa aviation 2022 forum, 3949, 2022
22022
Experimental and Numerical Analysis of Transient Erosion in Hybrid Rockets
M Rotondi, MT Migliorino, D Bianchi, L Kamps, H Nagata
Proceedings of the International Symposium on Space Technology and Science …, 2023
12023
T (H) RUST: applied research activities on liquid rocket propulsion at Sapienza University of Rome
F Nasuti, D Bianchi, MT Migliorino, M Grossi, M Fiore, M Rotondi, ...
Proceedings of the International Astronautical Congress, IAC, 2023
12023
Review and implementation of engineering models of rocket film cooling and nozzle erosion
SD Alessandro, P Concio, M Rotondi, D Bianchi, F Nasuti
Proceedings of EUCASS-3AF 2022, 2022
12022
Numerical and experimental analysis of capsules ablation and shape change including heating transient effects
M Rotondi, MT Migliorino, D Bianchi, P Pagani, A Turchi
AIAA Propulsion and energy 2020 Forum, 3969, 2020
12020
Small Satellite Hybrid Propulsion Systems: A Numerical Strategy for Regenerative Cooling Design
M Rotondi, L Kamps, H Shota, C Nguyen, G Gallo, H Nagata
AIAA SCITECH 2025 Forum, 1521, 2025
2025
Role of Multiphase Modeling on Nozzle Thermochemical Erosion in Solid Rocket Motors
M Rotondi, M Grossi, MT Migliorino, D Bianchi
AIAA Scitech 2023 Forum, 0392, 2023
2023
Transient Material Response Analysis of Carbon-based Thermal Protection Systems for Rocket Nozzle Applications
M Rotondi, MT Migliorino, D Bianchi
2nd International Conference on Flight Vehicles, Aerothermodynamics and Re …, 2022
2022
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