Marco Rotondi | Ricerc@Sapienza

Pubblicazioni

Titolo	Pubblicato in	Anno
Computational Analysis and Regression Laws for Nozzle Erosion Prediction in Hybrid Rockets	JOURNAL OF PROPULSION AND POWER	2024
Experimental and Numerical Analysis of Transient Erosion in Hybrid Rockets	Proceedings of the International Symposium on Space Technology and Science (ISTS)	2023
Role of Multiphase Modeling on Nozzle Thermochemical Erosion in Solid Rocket Motors	AIAA Scitech 2023 Forum	2023
T(H)RUST: applied research activities on liquid rocket propulsion at Sapienza University of Rome	Proceedings of the International Astronautical Congress, IAC	2023
Student firing tests and launches with commercial and self-made solid rocket motors	ACTA ASTRONAUTICA	2022
Review and Implementation of Engineering Models of Rocket Film Cooling and Nozzle Erosion	Proceedings of EUCASS-3AF 2022	2022
Numerical assessment of camphor ablation flight relevance in hypersonic wind-tunnel testing	JOURNAL OF SPACECRAFT AND ROCKETS	2022
Numerical analysis of carbon-based nozzle erosion including transient heating and shape change	Thermophysics. (2 vols) papers presented at the aiaa aviation forum 2022	2022
Transient Material Response Analysis of Carbon-based Thermal Protection Systems for Rocket Nozzle Applications	2nd International Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions and Engineering (FAR)	2022
Numerical Analysis and Wind Tunnel Validation of Low-Temperature Ablators undergoing Shape Change	INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER	2021
Numerical Analysis of Nozzle Transient Heating and Erosion in Hybrid Rockets burning HDPE	AIAA Propulsion and Energy Forum 2021	2021
Numerical Analysis of Nozzle Erosion in Hybrid Rockets and Comparison with Experiments	JOURNAL OF PROPULSION AND POWER	2021
Student firing tests and launches with commercial and self-made solid rocket motors		2021
Numerical analysis of nozzle heating and erosion in hybrid rockets and comparison with experiments	AIAA Propulsion and Energy 2020 Forum	2020
Numerical and experimental analysis of capsules ablation and shape change including heating transient effects	AIAA Propulsion and Energy 2020 Forum	2020