Gokmen Research
Independent advanced propulsion research initiative
Electric Propulsion

Electric propulsion.Built fromfirst principles.

Advancing ion and plasma propulsion systems for atmospheric flight, aerospace systems, and silent UAV architectures, from first-principles modelling to experimental hardware.

Research modelModel · Build · Test
Core domainsEHD · Plasma
Programme typeIndependent research
Program Evidence
2× National Finalist
KUF 2025 & 2026 · 3rd and 2nd place
50,000 NOK
Funded fellowship · laboratory and research budget
1 Published Preprint
engrXiv · DOI 10.31224/5626
3 Active Tracks
Diagnostics · EHD education · computational physics

Research focus.

Four connected lines of work spanning hardware, plasma behaviour, atmospheric propulsion, and mission-oriented applications.

01
Ionic Thruster Design

Empirical and analytical study of electrode geometry, collector radius, and spacing on thrust-to-power ratio in ionic wind generators — building on experimental prototypes toward optimised configurations.

02
Plasma Dynamics

Characterising ionisation, charge transport, and plasma sheath formation in low-temperature discharge environments relevant to electric propulsion and atmospheric flight.

03
Atmospheric Propulsion

Propulsion systems operating within planetary atmospheres — electrohydrodynamic (EHD) thrusters and hybrid plasma-aerodynamic mechanisms for silent, fuelless flight.

04
Defense & UAV Applications

Translation of electric propulsion research into low-observable, acoustically silent UAV platforms — where propulsion silence is a strategic capability, not just an engineering preference.

To develop the next generation of electric and plasma propulsion systems — grounded in rigorous physics, built in working hardware, and oriented toward applications that matter.
Work

Projects &
Publications

Ongoing and completed research spanning ionic thruster hardware, plasma diagnostics, propulsion analysis, and computational physics. Experimental systems are self-designed and physically built; theoretical tracks are identified explicitly.

Mar 2026–
ongoing
Ongoing · Furim Institutt
OES Diagnostics in Plasma Propulsor Efficiency

Developing a novel triad-method for assessing plasma propulsion efficiency using Optical Emission Spectroscopy. The approach aims to bring plasma propulsors one step closer to viable launch assistance by providing a richer diagnostic picture than single-instrument methods. Conducted under the Furim Institute Forward Looking Minds Fellowship.

Affiliation Furim Institutt
Methods OES · Python · Spectral Analysis
Apr 2026–
ongoing
Ongoing · Independent Research
Electrode Geometry and Efficiency in an Educational Model EHD Thruster

Developing an educational research paper addressing a gap in how fundamental EHD propulsion is taught, while investigating pin-to-ring electrode geometry and its effect on propulsor performance.

Focus Electrode Geometry · EHD Education
Methods Literature Review · Experimental Design · Academic Writing
Jan 2026–
ongoing
Ongoing · Independent
Quantum Wave Dynamics Analysis on a Representative EHD Thruster, Integrated PINN

An exploratory study applying quantum wave dynamics analysis to a representative electrohydrodynamic thruster model, integrated with a Physics-Informed Neural Network (PINN). The work sits at the intersection of quantum mechanics, plasma physics, and machine learning — pushing toward a more complete theoretical description of EHD propulsion phenomena.

Methods PINN · Quantum Mechanics · Neural Networks
Status In development
Feb 2025–
Jan 2026
Completed · Nesbru VGS · IB Extended Essay
Geometrical Optimisation of a Model EHD Ion Thruster and Resulting Efficiency in Terms of Thrust-to-Power

Extended essay and substantial improvement on prior work. Systematically investigated how electrode spacing and collector radius affect thrust-to-power ratio in a self-built EHD ion thruster — treating geometry as the primary design variable. Presented at KUF 2026 national finals.

Venue KUF 2026 · National Finals
Result 2nd Place — Naturvitenskap og Teknologi
Qualifies European Space Camp
2024
Completed · Research Proposal
Nanomaterial-Based Electrodes for Improved Plasma Propulsion Efficiency, in Aim of Achieving Space Launch

A research proposal investigating the use of nanomaterial-based electrodes as a route to substantially improved plasma propulsion efficiency. The proposal examines how engineered nanoscale electrode surfaces could reduce energy losses, enhance ionisation rates, and push the thrust-to-power ratio toward ranges relevant for space launch applications.

Type Research Proposal
Focus Nanomaterials · Electrode Design · Plasma Efficiency
Jan–Dec
2025
Power-to-Thrust Analysis: Investigating Feasibility of Ionic Thruster Performance for Space Launch

Investigated the power-to-thrust ratio of a self-designed and self-built small-scale ionic thruster. Explored scalability to traditional thruster sizes, validated experimental data against theoretical predictions, and examined potential optimisations for maximum thrust — ultimately assessing whether electric propulsion can serve as an alternative to chemical propulsion for space launch. Published as a preprint on engrXiv.

Venue KUF 2025 · National Finals
Result 3rd Place — Naturvitenskap og Teknologi
engrXiv · Engineering Archive · 2025
Power-to-Thrust Analysis: Investigating Feasibility of Ionic Thruster Performance for Space Launch

Investigates the power-to-thrust ratio of a self-designed and self-built small-scale ionic thruster. The study explores scalability to traditional thruster sizes, validates experimental data against theoretical predictions, and examines potential optimisations for maximum thrust. Estimates performance in vacuum environments and critically evaluates whether electrohydrodynamic propulsion can serve as a viable alternative to chemical propulsion for space launch — challenging the prevailing view that electric propulsion is unsuitable for launch-phase missions.

Author Said Zeki Gökmen
Published Dec 2025
License CC BY 4.0
Founder
Said
Zeki
Gökmen
Research & Teaching Fellow · Independent Researcher

Research & Teaching Fellow at FURIM Institutt and independent researcher building an early-stage propulsion programme around ionic and plasma systems. Current work spans atmospheric EHD hardware, Optical Emission Spectroscopy diagnostics, educational propulsion research, and physics-informed computational models.


Awarded a 50,000 NOK Forward Looking Minds Fellowship with laboratory space and a research budget. Previous engineering work at Merxcell included an AI-assisted aviation and MRO intelligence workflow, adding database and systems experience to the experimental research foundation.

Identity
Gökmen /ˈɡøk.mɛn/
From Old Turkic gök — sky or celestial — and men — one who embodies: he who reaches for the sky.
2026
KUF 2026 — 2nd Place, Naturvitenskap og Teknologi

National science competition. Project: electrode spacing and collector radius effects on thrust-to-power ratio in an ionic thruster. Qualifies for European Space Camp.

2026
European Space Camp — Qualified

Selected to attend European Space Camp following KUF 2026 placement. Annual programme hosted at Andøya Space Center, Norway.

2026
Furim Institute Forward Looking Minds Fellowship

50,000 NOK funded fellowship with laboratory space and a research budget, supporting independent plasma-propulsion research and STEM teaching.

2026
Research & Teaching Fellow — FURIM Institutt

Conducting research and development while teaching and presenting STEM topics in Oslo.

2025
KUF 2025 — 3rd Place, Naturvitenskap og Teknologi

National science competition. Project: power-to-thrust analysis of a self-built ionic wind generator.

2025
Published Preprint — engrXiv Engineering Archive

"Power-to-Thrust Analysis: Investigating Feasibility of Ionic Thruster Performance for Space Launch." DOI: 10.31224/5626. ORCID authenticated. CC BY 4.0.

Propulsion
Ionic / EHD thrusters
Electric propulsion
Thrust measurement
Scalability analysis
Plasma Physics
Ionisation kinetics
Plasma sheath theory
Charge transport
Low-temp discharge
Hardware
Thruster prototyping
HV electrode systems
Indirect force measurement
Experimental design
Analysis
Thrust-to-power ratio
Experimental validation
Theoretical modelling
Uncertainty analysis
Academic & Teaching
IB Diploma alumnus
STEM teaching
Scientific writing
Preprint publication
Systems & Software
Python workflows
AI-assisted research
Aviation databases
Technical intelligence
Join the work

Collaborate &
Connect

Gokmen Research is building a small, output-driven network of researchers working on plasma and electric propulsion. If your work touches any of the areas below, reach out.

Area 01
Plasma Propulsion Research

Researchers working on EHD thrusters, ion drives, Hall thrusters, or plasma sheath physics at any level — student, postdoc, or faculty. Output-oriented collaboration only.

Area 02
Computational & ML Methods

Physicists or engineers applying PINNs, CFD, or quantum simulation methods to propulsion or plasma problems. Active intersection with the quantum-EHD study underway.

Area 03
Diagnostics & Instrumentation

Experimentalists with OES, Langmuir probe, or thrust-stand experience. The OES triad-method project has immediate opportunities for co-authorship.

Area 04
UAV & Defense Applications

Engineers or analysts with interest in electric propulsion for low-acoustic UAV platforms. Translation of lab results into applied systems is a core long-term direction.

Send a brief note about your work and what kind of collaboration you have in mind. No formal pitch needed — a paragraph is enough.

Direct Email