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Information on didactic, research and institutional assignments on this page are certified by the University; more information, prepared by the professor, are available on the personal web page and in the curriculum vitae indicated on this webpage.
Information on professor
ProfessorGalfetti Luciano
QualificationAdjunct professor
Belonging DepartmentDipartimento di Scienze e Tecnologie Aerospaziali
Curriculum VitaeDownload CV (77.38Kb - 06/03/2020)
OrcIDhttps://orcid.org/0000-0002-6164-4665

Contacts
Professor's office hours
DepartmentFloorOfficeDayTimetableTelephoneFaxNotes
Scienze e Tecnologie Aerospaziali----FridayFrom 09:30
To 12:30
02.3399.8526--Ricevimento in altri giorni, previo accordo.
E-mailluciano.galfetti@polimi.it
Professor's personal website--

Data source: RE.PUBLIC@POLIMI - Research Publications at Politecnico di Milano

List of publications and reserach products for the year 2023
No product yet registered in the year 2023


List of publications and reserach products for the year 2022 (Show all details | Hide all details)
Type Title of the Publicaiton/Product
Conference proceedings
Development of Paraffin-Based Fuels for a Vortex Combustion Hybrid Rocket Engine (Show >>)
Numerical and Experimental Investigation of a Lab-Scale Paraffin Motor with Swirled Injection of Gaseous Oxygen (Show >>)
Reduction of Solid Propellants Environmental Impact: Al-Mg Mechanically Activated Fuels and AP-PSAN Blends (Show >>)
Thermite-For-Demise (T4D): Material Selection for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry (Show >>)
Thermite-for-Demise (T4D): Concept Definition for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry (Show >>)
Towards High-Performing Paraffin-Based Fuels Exploiting the Armored Grain Concept (Show >>)


List of publications and reserach products for the year 2021 (Show all details | Hide all details)
Type Title of the Publicaiton/Product
Journal Articles
Actualization of an efficient throttleable laser propulsion mode (Show >>)
Experimental evaluation of HTPB/paraffin fuel blends for hybrid rocket applications (Show >>)


List of publications and reserach products for the year 2020 (Show all details | Hide all details)
Type Title of the Publicaiton/Product
Contributions on scientific books
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation (Show >>)
Conference proceedings
Impact of 3d-printing on the mechanical reinforcement and the ballistic response of paraffin-based fuels: The armored grain (Show >>)
Journal Articles
A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain - Mechanical characterization (Show >>)
Effect of mechanical activation on the reactivity of composites for flameless heaters (Show >>)


List of publications and reserach products for the year 2019 (Show all details | Hide all details)
Type Title of the Publicaiton/Product
Conference proceedings
Activated and Nano-Sized Aluminum as Metal Fuels in Solid Rocket Propellants (Show >>)
Aerospace Propulsion Research Activities at SPlab. Overview and Results (Show >>)
An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part I, Mechanical and Pre-Burning Characterization (Show >>)
An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part II, Ballistic Characterization (Show >>)
Burning Behavior Investigation of a Vortex Flow Pancake Hybrid Rocket Engine (Show >>)
Effects of Aluminum Composites on the Regression Rates of Solid Fuels (Show >>)
Evaluation of a Ramjet Model in a Supersonic High-Enthalpy Tunnel (Show >>)
Experimental data from ramjet/scramjet combustion and numerical validation perspectives (Show >>)
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion (Show >>)
Green Fuels for Rocket Propulsion: Current Status and Future Perspectives of Paraffin-Based Formulations (Show >>)
Hydrogen-Based Thrusters for Supersonic and Hypersonic Flight: Experimental Characterization (Show >>)
Influence of Operating Parameters on the Ballistics of a Lab-Scale Vortex Flow Pancake Hybrid Rocket Engine (Show >>)
Mechanically Activated Al/Mg Powders for Solid Rocket Propellants (Show >>)
Particle Size in SRM Plume: Assessment of Collection Method (Show >>)
Particle Size in Solid Rocket Motor Plume: New Experimental Method (Show >>)
Performance and Environmental Impact Prediction of SRMs. Road Map for Reliable Dataset of Particles in Plume (Show >>)
Regression Rate and Combustion Efficiency in a Vortex-Flow Hybrid Rocket Engine (Show >>)
Trade-Off Analysis of a New Liquid Rocket Engine (Show >>)
Journal Articles
Accelerated ageing of micron- and nano-sized aluminum powders: Metal content, composition and non-isothermal oxidation reactivity (Show >>)
Aluminum powders: aging effects on metal content and thermogravimetry reactivity (Show >>)
Combustion Processes in Hybrid Rockets (Show >>)
Development of an intrusive technique for particles collection in rockets plume (Show >>)
Iron oxide as solid propellant catalyst: A detailed characterization (Show >>)
manifesti v. 3.5.10 / 3.5.10
Area Servizi ICT
21/09/2023