Master´s Thesis: Proportional Piezo Valve for Electric Propulsion Feed Systems (m/f/d)

München · Internship

Seed · $11.6M · 96d ago Posted 2d ago

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Why join deltaVision?

This could be huge if in-orbit refueling becomes routine, because every spacecraft and launcher would depend on the valves, pumps and fluid systems that make it work. A supply chain that delivers those parts reliably could anchor the whole space economy. deltaVision, a Munich aerospace manufacturer, closed a $12M seed, bigger than nearly two in three seed rounds this half, and it has 18 open roles, nine of them in engineering.

JustBacked's take, based on deltaVision's own site and its funding and hiring data.

Deine Mission

Join our fluid control equipment development team and help develop a proportional piezo valve for precise mass flow control in electric propulsion feed systems. Electric thrusters such as Hall-effect and gridded ion thrusters need a very stable, finely resolved propellant flow (typically xenon or krypton) in the low mg/s range.
Piezoelectric actuators offer fast response, high resolution, and low power use, which makes them a promising alternative to conventional thermal throttles and bang-bang solenoid regulation. However, effects such as hysteresis, creep, and temperature dependence must be understood and compensated. You will model, build up, and experimentally characterize a piezo-based flow control concept, and develop a control strategy for closed-loop mass flow regulation.

Your Responsibilities

Review the state of the art in mass flow control for electric propulsion, including thermal throttles, solenoid-based pressure regulation, and piezo valves
Research state of the art of piezo actuators and trade different architectures (e.g. stacked, amplified, piezo motors) for the given application
Characterize the piezo actuator (stroke, force, hysteresis, creep, temperature behavior) and its effect on the valve’s flow area
Assess the concept against typical electric propulsion requirements (flow range, leak rate, power consumption, operating temperature range)
Build a physical flow model of the valve that links actuator stroke, inlet pressure, and gas properties to mass flow, covering the relevant flow regimes (e.g., choked and transitional flow)
Integrate the actuator into a valve architecture and design a breadboard model
Review existing test bench infrastructure with pressure sensors and a mass flow meter, adapt if necessary, and carry out flow characterization with inert gases
Optionally, develop and implement a closed-loop control strategy (e.g., PID with hysteresis compensation) and evaluate its performance in terms of accuracy, resolution, response time, and stability
Optionally, derive design recommendations for a flight-representative valve

Dein Profil

Currently enrolled in a relevant engineering program, ideally Aerospace Engineering, Mechanical Engineering, Mechatronics, Electrical Engineering, or a similar field
Solid knowledge of fluid mechanics or gas dynamics; experience with control engineering is a plus
Hands-on experience with lab work, test setups, or measurement technology (e.g., from working student jobs, engineering projects, or student teams)
Programming skills in Julia, Python or MATLAB/Simulink for modeling, data analysis, and controller design
Motivated, pragmatic, and self-organized
Fluent in English; German and other languages are a plus

Wir bieten

Internship can be mandatory or voluntary
Above average remuneration
Guided but self-determined problem solving to realize your ideas
Deep dive into the domain of commercial spaceflight and mobility
Opportunity for an adjacent employment as working student or for thesis
Flexible entry date, the sooner the better with flexible working hours
Holiday entitlement above German standards