Matteo Fiore | Ricerc@Sapienza

Pubblicazioni

Titolo	Pubblicato in	Anno
Transient Analysis of Liquid Rocket Engine Chilldown and Startup by Conjugate Heat Transfer Approach	AIAA SciTech Forum and Exposition, 2024	2024
Module performance and heat transfer analysis of a clustered annular aerospike nozzle	Proceedings of the space propulsion conference 2024	2024
Modeling postcritical two-phase heat transfer in EcosimPro/ESPSS environment	Proceedings of the 9th Space Propulsion Conference	2024
Conjugate heat transfer numerical simulations of a methane-oxygen liquid rocket engine	Proceedings of the 2024 Space Propulsion Conference	2024
Cooling system design for an upper-stage aerospike	Proceedings of the 34th ISTS Conference	2023
Cooling system analysis of a clustered module aerospike for upper-stage applications	Proceedings of Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS	2023
CFD simulations of flow in LREs rectangular cooling channels	Proceedings of the 34th International Symposium on Space Technology and Science	2023
T(H)RUST: applied research activities on liquid rocket propulsion at Sapienza University of Rome	Proceedings of the International Astronautical Congress, IAC	2023
Conjugate heat transfer applied to transitory analysis for rocket engine cooling systems design	Materials Research Proceedings	2023
Modeling liquid rocket engine coolant flow and heat transfer in high roughness channels	AEROSPACE SCIENCE AND TECHNOLOGY	2022
HEM modeling for subcritical flows in liquid rocket engine cooling systems	Proceedings of the AIAA Aviation Conference 2022	2022
A design strategy for water-based noise suppression systems in liquid rocket engines firing tests	CEAS SPACE JOURNAL	2022
Analysis of coolant flow and heat transfer in highly rough channels for LRE	Proceedings of the 9th EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)	2022
Student Activities in Manufacturing and Launching Advanced Small-Scale Solid-Propellant Rockets		2022
Heat transfer prediction in rough cooling channels for liquid rocket engines	Proceedings of AIDAA 2021	2021
Design and evaluation of aerospike nozzles for an upper stage application.	Proceedings of the Space Propulsion Conference 2020+1	2021