Aleksander Gorgeri Email & Phone Number

Warsaw, Pl

Warsaw, Mazowieckie, Poland

Lead role in multiple propulsion related activities, mainly in the domain of green propulsion. Development of green hypergolic fuel combinations, reaction control thrusters as well as novel cryogenic propulsion systems for interplanetary usage.Responsibilities:-Managing ESA as well as national (NCR&D) propulsion related activities (TRL level 4/5).-Leading teams of up to 10 engineers.-Planning and supervising testing campaigns.-Communicating with ESA as well as national technical staff.

Warsaw, Mazowieckie, Poland

Designing, integrating and testing combustion chambers of various types with an emphasis on thermo-structural analyses. Implementation of additive manufacturing into chambers' design through cooperation with internal manufacturing center.Responibilities:-Designing bipropellant rocket engines' combustion chambers (regenerative, radiative, heat-sink).-Performing thermo-structural and fatigue analyses of combustion chambers.-Developing in-house FEM software for combustion chambers' thermo-structural analyses as well as Inverse Heat Transfer problems.-Assistance in engine testing with regards to chamber operations (test planning, data analysis).

Warsaw, Mazowieckie, Poland

Responsibilities:-Performing heat transfer and combustion analysis in hybrid and liquid fueled rocket engines.-Creating preliminary designs of hybrid and liquid fueled rocket engines.-Conducting research on the combustion of polymer-based fuels in hybrid rocket engines.-Designing and integrating feed systems for hybrid and liquid fueled rocket engines.-Planning and supervising testing campaigns rocket engines and their subsystems.

Warsaw, Mazowieckie, Poland

Responsibilities:-Leading design teams of up to 5 people.-Management of the projects' finances, contact with subcontractors.-Representing the Rocketry Division at conferences and competitions.

Warsaw, Mazowieckie, Poland

Responsibilities:-Internal ballistics analysis of a solid-propellant rocket engine.-Numerical analysis and mechanical design of a solid-propellant rocket engine pyrotechnic igniter.

Msc, Mechanical Engineering

Thesis: Heat flux analysis and inverse heat transfer validation of a 5kN hypergolic rocket engine combustion chamber Interim thesis.

Bsc, Aerospace Engineering

Activities and Societies: Koło Naukowe Napędów "MELprop"Thesis: Design and experimental evaluation of hybrid rocket engine Interim thesis.