Athens, Greece · Propulsion / launch vehicles
I connect propulsion, aerodynamics, structures, and flight data into one engineering argument—then test where that argument meets reality.
01 / Selected work
Each case study is structured for a fast technical review: requirement, contribution, method, and result.
Featured research · end-to-end vehicle design
An integrated design study linking propulsion, aerodynamics, stability, structures, recovery, simulation, and measured flight behaviour in one traceable engineering chain.
Internal ballistics · pressure vessel · thermal
Coupled burn-rate and chamber-pressure modelling with pressure-vessel sizing, closure checks, transient wall heating, and conservative design margins.
Stability · wave drag · flutter
A parametric search over aspect ratio, taper, root chord, sweep, and thickness, screening candidates against static-margin and aeroelastic limits.
Avionics selection · recovery · data reconciliation
Selected and integrated a flight computer, defined the recovery sequence, and reconciled logged flight data with a bracketed simulation model.
Open-source adaptation · mechatronic integration
Built from the Open5X architecture and adapted through targeted mechanical and process modifications, with emphasis on integration and practical commissioning.
CNC · controls · fabrication
Add the design objective, your exact contribution, two engineering decisions, and one measured outcome. Keep this card only if it strengthens the role you are targeting.
02 / Research
The thesis is positioned as the central research artifact—not just a long report, but a traceable record of assumptions, models, design choices, and verification.
Undergraduate thesis · [Add university / department]
A practical, theory-backed development framework intended to help small research groups translate a payload objective into a complete sounding-rocket design. [Replace with your final 60–90 word abstract.]
03 / Profile
Propulsion is the destination; multidisciplinary vehicle design is the working language.
Short professional profile
My work is strongest where analytical models meet real design constraints: pressure, temperature, stability, mass, manufacturing, and test evidence. I value clear requirements, honest margins, and results that another engineer can audit.
Replace this paragraph with a 70–100 word biography tailored to the roles you are applying for.
[University / department] · Thesis focus: sounding-rocket systems and propulsion.
[Organisation] · One sentence on scope, ownership, and measurable contribution.
Include only if it adds evidence that is not already obvious from the projects above.
04 / Contact
For propulsion, aerospace R&D, flight systems, and early-career engineering opportunities.