| 04-M07-FP-2515 | Studentenprojekt zur Simulation von Raumfahrt Systemen (S4) [SysEng] Anmeldung im Stud.IP bis: 15.10.2025
Projektauftakt am: 22.10.2025
max. Gruppengröße: 3
Ansprechperson: Jens Grosse, jens.grosseprotect me ?!zarm.uni-bremenprotect me ?!.de
In this project students shall implement new simulation approaches for the design of space systems. In this project phase from winter semester 2025 and summer semester 2026 the focus is on a simulation of the hypersonic ascent of a sounding rocket with CFD and potential assistance through AI. The students will work on one of the following topics:
1.) Ablative heat shield implementation on available nose cone models with atmospheric parameters investigation
2.) Training of AI algorithm / neural network on different data sets obtained from a classical CFD simulation | Dr.-Ing. Jens Große |
| 04-M07-FP-2514 | Studentenprojekt zur Untersuchung und Entwicklung von Enabling Technologies für Quantensensoren (QTech) [SysEng] Anmeldung im Stud.IP bis: 15.10.2025
Projektauftakt am: 22.10.2025
Ansprechperson: Jens Grosse, jens.grosseprotect me ?!zarm.uni-bremenprotect me ?!.de
The ZARM institute investigates multiple quantum sensor for sensing of accelerations or pressures, as well as different approaches to provide frequency references.
This project will study different enabling technologies supporting the developments of these quantum sensors and frequency references. Hereby the participants will get a basic introduction into fundamentals of quantum technologies and will subsequently work on one of the following topics:.
- Design and comissioning of a teststand for Partial Pressure determination of Potassium using Spectroscopy
- Design and test of a micro valve for UHV systems
| Dr.-Ing. Jens Große |
| 04-M30-MP-2555 | Durchführbarkeit des Haber-Bosch Prozesses für die Ammoniasynthese unter Mars Bedingungen The Haber-Bosch process is an indispensable part of the modern chemical industry, enabling large scale ammonia production particularly for fertilizers. Its potential (…) The Haber-Bosch process is an indispensable part of the modern chemical industry, enabling large scale ammonia production particularly for fertilizers. Its potential implementation on Mars is of significant interest for supporting long-term human exploration through in-situ resource utilization (ISRU). This literature based project investigates the feasibility of deploying Haber-Bosch ammonia synthesis under Martian environmental conditions, with a particular focus on comparing key process parameters between Earth and Mars.
Students will systematically analyze differences in nitrogen availability, hydrogen sourcing, operating pressure, temperature requirements, and overall energy demand. The Martian atmosphere, composed predominantly of CO₂ and only about 2 % nitrogen, presents significant challenges for nitrogen extraction and compression. In contrast to Earth, where hydrogen is primarily derived from fossil fuels, Martian hydrogen production relies on energy-intensive water electrolysis from sub surface ice deposits or hydrated minerals. With the core reaction conditions of the Haber-Bosch process remaining unchanged, the additional energy requirements associated with gas capture, purification, and high-pressure compression are expected to substantially increase the total system energy demand on Mars. The project will further evaluate potential energy sources, including solar power, and assess their suitability for sustaining ammonia production. | Prof. Dr. Katharina Brinkert |
| 04-M30-MP-2552 | Elektrochemische CO2 Reduktion im Weltraum: Vom Abfallprodukt zur Treibstoff- und Lebenserhaltungssystemressource Crewed spacecraft and surface habitats continuously produce CO₂ as a metabolic byproduct, which must either be scrubbed and vented or actively converted into useful (…) Crewed spacecraft and surface habitats continuously produce CO₂ as a metabolic byproduct, which must either be scrubbed and vented or actively converted into useful products. Electrochemical CO₂ reduction reaction (CO₂RR) offers a dual benefit: removing a cabin atmosphere contaminant while producing valuable chemicals such as carbon monoxide, methane, formate, or methanol that can serve as fuel precursors or feedstocks for further synthesis. This literature project examines the electrochemical reduction of CO₂ as a component of a closed-loop life support and ISRU strategy, with particular attention to how microgravity and the CO₂-rich Martian atmosphere alter the design requirements relative to terrestrial systems.
Students will survey catalyst materials and selectivity for relevant CO₂RR products, review existing space-heritage carbon dioxide removal systems such as the Sabatier reactor on the ISS, and assess how an electrochemical approach compares in terms of mass, power consumption, and product flexibility. Simple Faradaic efficiency and power budget calculations will be performed to estimate the CO₂ conversion rate achievable within the electrical power envelope of a Mars surface habitat. The project will equip students to critically evaluate CO₂RR as a candidate technology for integration into future closed-loop planetary life support architectures. | Prof. Dr. Katharina Brinkert |
| 04-M09-MW-P-2502 | Elektrolyseur-Designstrategien für Weltraumanwendungen ECTS: 15 (MSc. SpaceEng 12) Die elektrochemische Wasserspaltung (2 H2O → 2 H2 + O2) ist sowohl für die terrestrische Wasserstoffproduktion – als Grundlage zukünftiger Energiespeichertechnologien (…) Die elektrochemische Wasserspaltung (2 H2O → 2 H2 + O2) ist sowohl für die terrestrische Wasserstoffproduktion – als Grundlage zukünftiger Energiespeichertechnologien – als auch für die extraterrestrische Sauerstoffproduktion für Lebenserhaltungssysteme in Weltraummissionen, z. B. das Oxygen Generator Assembly auf der ISS, von entscheidender Bedeutung. Extraterrestrische Faktoren wie Mikrogravitation, Strahlungsexposition und extreme Temperaturschwankungen beeinflussen die Leistung von Elektrolyseuren im Vergleich zu erdgebundenen Systemen. In Schwerelosigkeit wird die Phasentrennung zwischen Elektroden, flüssigem Elektrolyten und gasförmigen Produkten erschwert, da keine Auftriebskräfte auftreten. In diesem Literaturprojekt werden die Unterschiede in Elektrolyseur-Designs für terrestrische und Weltraumanwendungen untersucht, mit Schwerpunkt auf Effizienz, Langlebigkeit und Leistungsfähigkeit. Ziel des Projekts ist wertvolle Erkenntnisse zur Optimierung zukünftiger Elektrolyseur-Technologien für den Einsatz unter Schwerelosigkeit mittels der Analyse von bereits etablierten Elektrolyseur-Designs, Materialauswahlstrategien und bekannten Prozessherausforderungen zu gewinnen. | Prof. Dr. Katharina Brinkert |
| 04-M09-LT-P-2551 | Evaluation der Nutzung von IR-Kameras als neues Messverfahren zur Erkennung vom Strömungsabriss am Tragflügel ECTS: MScPT: 15, MScSpaceEng: 12 Entwicklung einer Machbarkeitsstudie zum Einsatz von
Thermalkameras zur Erkennung vom Strömungsabriss am
Tragflügel eines Ultraleichtflugzeuges Entwicklung einer Machbarkeitsstudie zum Einsatz von
Thermalkameras zur Erkennung vom Strömungsabriss am
Tragflügel eines Ultraleichtflugzeuges | Dr. Florian Meyer |
| 04-M30-MP-2551 | Kreisläufige Lebenserhaltungssysteme für die Weltraumerforschung The C.R.O.P (Combined Regenerative Organic Food Production) technology was based on sustainable practices that integrate circular resource use into space systems. This (…) The C.R.O.P (Combined Regenerative Organic Food Production) technology was based on sustainable practices that integrate circular resource use into space systems. This system relied on natural biological processes, where micro-organisms convert components of urine into plant fertilizers. These fertilizers are then used to grow crops in controlled environments, contributing to food production while simultaneously managing waste. This integration of waste recycling and agriculture aimed to reduce the need for continuous resupply from Earth, which is one of the major challenges in space exploration. Developed and demonstrated in experiments such as the Eu: CROPIS mission by the German Aerospace Centre (DLR), this approach focused on converting human waste into a usable fertilizer for plant cultivation. Rather than treating waste as a disposal problem, C.R.O.P utilized it as a valuable resource, aligning with the principles of closed-loop life support systems that are essential for long-duration extra-terrestrial missions to the Mars.
In this project, students will analyse how systems like C.R.O.P function, compare them with other existing space fertilizer development strategies, and assess their advantages and limitations in space environments. They will also be encouraged to think creatively by proposing simple conceptual designs for closed-loop fertilizer systems tailored to Martian habitats. By the end of the project, students will have developed the ability to critically engage with interdisciplinary research and appreciate the role of sustainable technologies in shaping the future of space exploration. | Prof. Dr. Katharina Brinkert |
| 04-M30-MP-2553 | Lichtassistierte Wasserstoffproduktion auf der Mond- und Marsoberfläche: Eine Ressourcen- und Powerbudgetanalyse In-situ resource utilization (ISRU) on the Moon and Mars relies on the ability to generate and store chemical energy from locally available resources, most notably (…) In-situ resource utilization (ISRU) on the Moon and Mars relies on the ability to generate and store chemical energy from locally available resources, most notably water ice and solar irradiance. Photoelectrochemical (PEC) and photovoltaic-coupled electrolysis (PV-E) systems have been proposed as compact, scalable routes to producing hydrogen and oxygen from surface water without continuous resupply from Earth. This literature project compares PEC and PV-E architectures for solar hydrogen production under extraterrestrial conditions, examining how reduced solar flux, dust accumulation, and day-night cycles constrain system design on the lunar surface versus Mars.
Students will survey efficiency benchmarks reported for state-of-the-art PEC devices under terrestrial and simulated space conditions and assess how radiation degradation of semiconductor photoelectrodes impacts long-term performance. Back-of-envelope calculations will quantify the required solar collector area, electrolyser power rating, and hydrogen storage volume to sustain oxygen production for a four-person surface habitat over a 500-day mission at both locations. The project provides students with an integrated perspective on the interdependencies between solar energy conversion, electrochemistry, and ISRU mission architecture. | Prof. Dr. Katharina Brinkert |
| 04-M30-MP-2554 | Thermisches Management von elektrochemischen Systemen in der Weltraumumgebung Electrochemical systems such as water electrolysers and fuel cells are critical components of closed-loop life support systems for long-duration space missions. On (…) Electrochemical systems such as water electrolysers and fuel cells are critical components of closed-loop life support systems for long-duration space missions. On Earth, convective heat dissipation passively assists thermal regulation. In microgravity, the absence of natural convection fundamentally alters heat and mass transfer at electrochemical interfaces. This literature project investigates thermal management strategies for electrochemical energy systems operating under space-relevant conditions, including microgravity, Lunar, and Martian surface environments. Students will review how the operating temperature affects the electrolyser efficiency, membrane durability, and electrolyte conductivity, and compare passive versus active thermal control approaches applicable to spacecraft volume and mass constraints.
Simple steady-state heat balance calculations will be performed to estimate acceptable operating power envelopes under representative mission scenarios (ISS, Lunar Gateway, Mars surface habitat). By the end of the project, students will be able to quantitively assess the feasibility of electrochemical life support components under thermal constraints and propose design guidelines for thermally robust space electrochemical systems. | Prof. Dr. Katharina Brinkert |
