Student theses at IRS
The theses are sorted by subject area / topic. Further information on the topic and the requirements can be found in the linked files. Please send applications to the respective contact person noted in the document.
Please note the guidelines for the processing and supervision for theses (As of October 2024) at the Institute for Space Systems.
The Latex-Code of this template can be downloaded here:
https://ncext.irs.uni-stuttgart.de/index.php/s/ijcF3z7mgenK9Le
Password: RaumfahrtMachtSpass.2025
Current student theses
Human Spaceflight and Exploration
Bachelor's Theses
The next generation of human space exploration missions will necessitate increasingly sophisticated Life Support Systems (LSSs) to ensure astronauts stay alive, healthy and happy. These LSSs come with a variety of individual challenges, complexity and dynamic behavior. To further enable development of individual subsystems in the context of a modular LSS, a small-scale LSS is constructed at the Institute of Space System. The test rig will consist of three chambers, with the main focus of this work being on the Habitat Chamber (HC) to simulate spacecrafts, stations or habitats. Due to the modular approach, many different variations of experiment placement at the HC flanges are possible.
This thesis aims to provide a first insight into the spatial distribution of gases inside the HC. Areas of high or low density, possible problems due to experiment configurations and the optimal placement of the inside fan and heater should be analyzed. The goal is to provide a recommendation for good sensor placement independent of configuration and identify operational limitations for the use of the HC.
| Type: | Bachelor Thesis |
|---|---|
| Acquirement: | • Familiarization with LSSs • Research on CFD simulations • Implementation of a CFD simulation pipeline for the HC • Simulation of gas distribution inside the HC with different configurations • Evaluation of results & recommendation on component placement • Documentation |
| Organisation: | Human Spaceflight and Exploration (060515) |
| Supervisor: |
|
| Examiner: | Claas Olthoff E-mail |
| Link: | To C@MPUS |
Master's Theses
The next generation of human space exploration missions will take crews farther away from Earth than ever before. These missions will necessitate increasingly sophisticated Life Support Systems (LSSs) to ensure astronauts stay alive, healthy and happy. Mission scenarios of this kind therefore require greater autonomy, relying on simulations as well as laboratory setups to recreate the nominal behaviour of the LSS during all mission phases.
In order to be able to simulate these complex LSSs at the Institute of Space Systems (IRS), a small-scale laboratory model of a LSS is being constructed. Since such a complex undertaking requires detailed planning, a Model Based Systems Engineering (MBSE) approach is suggested to optimize the development process. This approach can also be combined with a Digital Twin of the laboratory model that is currently being implemented at the IRS.
This thesis explores MBSE for developing a Life Support System from the ground up. It covers foundational knowledge of MBSE and Requirements Engineering, reviews relevant tools and system architecture, examines integrating MBSE with the Digital Twin, and evaluates the resulting approach.
| Type: | Master Thesis |
|---|---|
| Acquirement: | • Literature Research • Familiarization with MBSE Tools • Design of a MBSE approach for a Life Support System • Combination of MBSE and a Digital Twin • Implementation of the MBSE approach • Evaluation of the Approach |
| Organisation: | Human Spaceflight and Exploration (060515) |
| Supervisor: | |
| Examiner: | Claas Olthoff E-mail |
| Link: | To C@MPUS |
The next generation of human space exploration missions will require increasingly sophisticated life support systems (LSS) to sustain crews on long-duration missions far from Earth. V HAB, a powerful simulation system for modeling complex LSS, employs a unique bottom-up approach that allows for high-precision modeling of all LSS components up to a user-defined granularity. This approach enables V HAB to maintain high modeling accuracy by providing detailed information on mass flow, temperature, pressure, humidity, and composition for each individual process and subsystem.
Currently, V HAB operates entirely within MATLAB without requiring additional packages or toolboxes. It offers a library of pre-defined basic LSS components, allowing users to integrate existing subsystems into their designs rather than starting from scratch. However, V HAB lacks a user-friendly graphical interface. (GUI), hindering its accessibility and usability, especially for new users. This master's thesis will work in parallel with the ongoing development of the V HAB GUI to compare the suitability of Synera as an alternative approach.
Synera, a modern low-code automation platform, offers the potential to address these gaps and enhance V HAB's capabilities. The integration of V HAB with Synera provides significant potential to improve the functionality and user experience of the LSS modeling platform. By leveraging Synera's capabilities, the integrated system could provide a user-friendly graphical interface, streamline the design process with quick options and arranging tools, and offer real-time feedback through automated logic tests and live updating feeds. These features would make V HAB more accessible to new users while providing comprehensive overviews of designed LSS and enhancing understanding of their operations.
This master's thesis aims to investigate and implement this integration, creating an advanced modeling platform that enables more efficient data generation, improved visualization of simulation results, and enhanced automation of modeling workflows.
| Type: | Master Thesis |
|---|---|
| Acquirement: | • Familiarization with LSS technologies, V HAB's architecture, and Synera's features • Develop a conceptual framework for integrating V HAB simulations within Synera • Implement custom nodes in Synera for V HAB operations and LSS components • Design and implement a user-friendly graphical interface for V HAB using Synera • Conduct a case study of a complex LSS scenario using the integrated V HAB-Synera platform • Evaluate the integrated system's performance • Documentation |
| Organisation: | Human Spaceflight and Exploration (060515) |
| Supervisor: | |
| Examiner: | Claas Olthoff E-mail |
| Link: | To C@MPUS |
Satellite Technology
EIVE
With the 6-unit CubeSat EIVE, the first in-orbit verification of a communication link in the E-band is planned.
Currently, there are no open theses.
ESBO DS
The "Design Study for the European Stratospheric Balloon Observatory" ESBO DS is a research infrastructure project designed to pave the way for an astronomical observatory based on stratospheric balloons.
The topics can be adapted for a Bachelor's or Master's thesis. Please clarify further details with the respective contact persons.
Currently, there are no open theses.
Flying Laptop
The small satellite Flying Laptop is the first satellite of Stuttgart's small satellite program and is still fully operational in orbit.
Master's theses
Cosmic Dust
Cosmic dust is understood to mean omnipresent tiny particles in space consisting of agglomerates of just a few molecules up to particles a few 100 μm in size. The cosmic dust working group at the IRS examines these particles with the help of self-made sensors installed on space probes.
Bachelor's & Master's theses (both possible)
- Implementation and test of an HVI experimental setup for ice-dust samples at the dust accelerator
- Development of a software application for the implementation and execution of space projects (05/2025)
- Development of a machine learning model for local application on a scientific instrument (Edge AI) for the in-situ detection of cosmic dust (05/2025)
- MOLFLOW space: Modeling of chemical cross contamination in Space (09/2025)
Master's theses
ROMEO
ROMEO "Research and Observation in Medium Earth Orbit" is a 60 kg small satellite that is planned to be operated in an elliptical orbit at an altitude of up to 3000 km. In addition to technology demonstrations by the Institute for Space Systems, its mission will be the research of the Earth's climate and radiation environment.
Possible as Bachelor's and Master's theses
- Systems Theoretic Process Analysis of the Flight Software of the small satellite ROMEO (01/26)
- Other topics for Subsystem Simulation
- Integration einer Orbit-Simulation in eine Flugdynamik-Software für den Satellitenbetrieb (12/25)
SOURCE
Space robotics
The space robotics group develops rover systems for the exploration of planetary surfaces. The focus is on the development of rover chassis systems and technologies that can still be used under demanding conditions on planetary surfaces.
Currently, there are no open theses.
Other
Bachelor's theses
Master's theses
Space
Transportation
Technology
Mission and System Analysis
Bachelor's theses
Master's theses
Collaborative Research Center 1667 ATLAS
Bachelor's theses
Master's theses
- Development of a Langmuir time of flight probe for velocity measurements in oxygen plasmas (05/2025)
- Development of a transient differential heat flux probe for measurements of atomic oxygen
fluence (05/2025) - Satellite Aerodynamics and Orbit Control
- Negative Ion Beamline
Bachelor or Master's theses
- Optimization of Ground Station Networks for Reliable Communication with VLEO Satellites (12/2025)
- Development of a FMECA Framework for VLEO Satellite Mission Operations (12/2025)
- Feasibility Study on Using SatNOGS to Improve Orbit Predictions for VLEO Satellites (12/2025)
- Investigation on Ground Station Modifications for VLEO Satellite Mission Support (12/2025)
- Development of a Flight Dynamics System for VLEO Satellite Operations Using Orekit (12/2025)I
Plasma wind tunnels and space propulsion systems
Bachelor's theses
- Plasma-based Extraction of Solid Carbon from Atmospheric CO2
- Space Ruggedizing the IceBrain-1 IOT Node
Master's theses
- Enhancement of the Design Process of an RF Birdcage Antenna for a Helicon-based Plasma Thruster (03/2025)
- Simulation and Design of an improved Magnet Configuration for an RF Helicon-based Plasma Thruster (02/2025)
- System Requirement Study of an Active Magnetic Shield for High Enthalpy Earth Entry (02/2025)
- Training Image Generator for the IceBrain-1 Image Recognizer AI
- Größen- und Leistungsskalierung einer existierenden Sauerstoff-Methan-Verbrennung einer innovativen 60 kN-Hyperboloid-Flüssigraketenbrennkammer hin zur Wasserstoffperoxid-Kerosin-Verbrennung der 2,5 kN Schubklasse in Ansys-Fluent
Sensorics
Bachelor's theses
- Implementation of real-time image recognition for optical accuracy enhancement in inkjet printing
- Development of a test rig for the characterization of hydrogels for bionic sensors
Master's theses
- Numerical simulation of transient transport processes of ions in electrolytes
- Optimization of an artificial lipid membrane for biosensors
- Implementation of real-time image recognition for optical accuracy enhancement in inkjet printing
- Development of a test rig for the characterization of hydrogels for bionic sensors
- Development of a tool to simulate the transient 2D diffusion of cations along a concentration gradient with variable geometry