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Information on didactic, research and institutional assignments on this page are certified by the University; more information, prepared by the lecturer, are available on the personal web page and in the curriculum vitae indicated on this webpage.
Information
LecturerParavan Christian
QualificationAssociate professor full time
Belonging DepartmentDipartimento di Scienze e Tecnologie Aerospaziali
Scientific-Disciplinary SectorIIND-01/G - Aerospace Propulsion
Curriculum VitaeDownload CV (448.51Kb - 20/10/2023)
OrcIDhttps://orcid.org/0000-0001-6558-8456

Contacts
Office hours
DepartmentFloorOfficeDayTimetableTelephoneFaxNotes
Dipartimento di Scienze e Tecnologie Aerospaziali---Space Propulsion Laboratory (SPLab), Ed. B16A---From :
To :
0223998068---Appointment is scheduled by email.
E-mailchristian.paravan@polimi.it
Personal website---

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

List of publications and reserach products for the year 2025 (Show all details | Hide all details)
Type Title of the Publicaiton/Product
Journal Articles
Thermite-for-demise (T4D): experiments and numerical modelling on solar array drive mechanism mock-ups containing thermite in an arc-heated wind tunnel (Show >>)


List of publications and reserach products for the year 2024 (Show all details | Hide all details)
Type Title of the Publicaiton/Product
Conference proceedings
Combustion in a Non-Conventional Hybrid Rocket Engine: Lab-Scale Testing of a Vortex Flow Pancake (Show >>)
Experimental Verification of Advanced Hybrids Performance and Scaling (Show >>)
Green Solid Fuels with Enhanced Mechanical Properties: Sustainable Waxes and Scale-Up Analysis of Armored Grains (Show >>)
Hydrolytic Space Propulsion: a New Opportunity for CubeSat Missions (Show >>)
Innovative Methodology for Evaluating Combustion Efficiency in Swirled Rocket Engines (Show >>)
Liquid Film Cooling: Advanced Modeling and Efforts Towards Validation (Show >>)
Testing Advanced Green Thermoplastic Fuels in a Vortex Hybrid Rocket Engine (Show >>)
Thermite-for-Demise (T4D): from Material Selection to Test Campaign (Show >>)
Journal Articles
Experimental Investigation of a H2O2 Hybrid Rocket with Different Swirl Injections and Fuels (Show >>)
Thermite-for-demise (T4D): Experiments and numerical modelling on ball-bearing unit mock-ups containing thermite in an arc-heated wind tunnel (Show >>)


List of publications and reserach products for the year 2023 (Show all details | Hide all details)
Type Title of the Publicaiton/Product
Conference proceedings
Ballistic Characterization of Armored Grains with Vortex Flow Pancake Hybrid Rocket Engine (Show >>)
Boosting Green Propellants: the Sustainable Armored Grain for Hybrid Rocket Propulsion (Show >>)
Diagnostic Techniques for Regression Rate of Paraffin-Based Fuels in a VFP Hybrid Rocket Engine (Show >>)
Effects of Grain Cracks on the Combustion of a VFP Engine Burning Paraffin-based Fuels (Show >>)
Experimental activities on the paraffin-based fuel MTM in the framework of the PHAEDRA project (Show >>)
Lab-Scale Investigation of Metal Hydrides as Solid Fuel Additives for Hybrid Rocket Propulsion (Show >>)
Liquid Film Cooling: Open-Literature Review, Modeling and Efforts Towards Validation (Show >>)
Paraffin-Based Fuels: Perspectives from Different Reinforcing Strategies and Metal Additives (Show >>)
Thermite-for-Demise (T4D): Preliminary Assessment on the Effects of a Thermite Charge in Arc-Heated Wind Tunnel Experiments (Show >>)
Thermite-for-Demise: Preliminary on-Ground Heat Transfer Experimental Testing (Show >>)
Journal Articles
A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain - Ballistic characterization (Show >>)
Numerical and experimental analysis of fuel regression rate in a lab-scale hybrid rocket engine with swirl injection (Show >>)
Test Activities on Hybrid Rocket Engines: Combustion Analyses and Green Storable Oxidizers - A Short Review (Show >>)


List of publications and reserach products for the year 2022 (Show all details | Hide all details)
Type Title of the Publicaiton/Product
Conference proceedings
Cellular Structures for Solid Fuel Grain Reinforcement: Mechanical and Combustion Performance in Conventional and Non-Conventional Hybrid Rocket Engines (Show >>)
Development of Paraffin-Based Fuels for a Vortex Combustion Hybrid Rocket Engine (Show >>)
Effects of Vortex Flow Pancake Hybrid Rocket Engine Operating Parameters on Liquefying Fuel Combustion (Show >>)
Hybrid Propulsion System for Future Rocket Applications (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
Conference proceedings
Liquefying Fuel Combustion in a Lab-scale Vortex Flow Pancake Hybrid Rocket Engine (Show >>)
Strategies for Paraffin-based Fuels Reinforcement: 3D Printing and Blending with Polymers (Show >>)
Journal Articles
Experimental evaluation of HTPB/paraffin fuel blends for hybrid rocket applications (Show >>)
Nickel acetylacetonate as decomposition catalyst for HTPB-based fuels: Regression rate enhancement effects (Show >>)
manifesti v. 3.9.3 / 3.9.3
Area Servizi ICT
27/04/2025