Mario Tindaro Migliorino

Pubblicazioni

Titolo Pubblicato in Anno
Role of Multiphase Modeling on Nozzle Thermochemical Erosion in Solid Rocket Motors AIAA Scitech 2023 Forum 2023
Numerical and Experimental Analysis of a Paraffin-based 1000 N Thrust Class Hybrid Rocket including Nozzle Erosion AIAA Scitech 2023 Forum 2023
Study, development, implementation and testing of a water resistojet propulsion system for CubeSats Proceedings of the International Astronautical Congress, IAC 2023
Convective and Radiative Wall Heat Transfer Evaluation in Film-Cooled Liquid Rocket Thrust Chambers Proceedings of the International Astronautical Congress, IAC 2023
Surrogate Neural Network Model for Integrated Ascent Trajectory Optimization of Throttleable Hybrid Rockets Proceedings of the International Astronautical Congress, IAC 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
Graphite Nozzle Erosion Trends in Paraffin/Oxygen Hybrid Rockets JOURNAL OF PROPULSION AND POWER 2022
Modeling of Wall Heat Flux in Oxygen-Methane Liquid Rocket Thrust Chambers AIAA AVIATION 2022 Forum 2022
Numerical estimation of nozzle throat heat flux in oxygen-methane rocket engines JOURNAL OF PROPULSION AND POWER 2022
Surrogate neural network for rapid flight performance evaluation of hybrid rocket engines JOURNAL OF SPACECRAFT AND ROCKETS 2022
Numerical assessment of camphor ablation flight relevance in hypersonic wind-tunnel testing JOURNAL OF SPACECRAFT AND ROCKETS 2022
Numerical simulations of fuel shape change and swirling flows in paraffin/oxygen hybrid rocket engines AEROTECNICA MISSILI E SPAZIO 2022
Numerical and experimental investigation of a lab-scale paraffin motor with swirled injection of gaseous oxygen Proceedings of the 9th EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) 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
Numerical Simulations of Fuel Shape Change in Paraffin-Oxygen Hybrid Rocket Engines AIAA Aviation Forum 2022
Student Activities in Manufacturing and Launching Advanced Small-Scale Solid-Propellant Rockets 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
Film cooling modeling in liquid rocket thrust chambers AIAA propulsion and energy forum 2021-3574 2021
Numerical Analysis and Wind Tunnel Validation of Low-Temperature Ablators undergoing Shape Change INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER 2021

ERC

  • PE8_1

Interessi di ricerca

Hybrid Rocket Engines, Computational Fluid Dynamics, Liquid Rocket Engines, Hypersonic Reentry

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