MBSE-based integration and variation of cryogenic hydrogen tank systems for future aircraft configurations

In MIWa, we develop a digital system model both for the integration of hydrogen cryogenic pressure tank systems into an aircraft and for the design and benchmarking of different variants. The requirements, system properties and dependencies will be modeled and the data models created will be linked to 3D geometry models as well as simulation models. Based on the system model, a virtual environment will be developed to visualize various cabin layouts and new systems, including the hydrogen tank system, as they are integrated into the aircraft. Thus, design variants can be geometrically analyzed and evaluated in a virtual world.