Streamlining the Aircraft Conceptual Design Process. From Concept to Flight: Streamlining the Aircraft Conceptual Design Process through Advanced Mass and Balance Techniques

Abstract

This master thesis investigates mass and balance techniques in the conceptual design phase of aircraft, with a focus on the ES-30 electric aircraft developed by Heart Aerospace. The thesis centers on developing and validating a computational tool for precise calculation of mass properties and center of gravity (CG) envelopes. This tool facilitates adjustments in aircraft design and has been applied to a case study on a conceptual liquid hydrogen (LH2) aircraft. The process aims to reduce the iterations needed in design modifications, speeding up the pre-flight testing phase and ensuring adherence to safety and performance standards. The findings demonstrate the tool’s applicability in future aircraft design projects, particularly for integrating new propulsion technologies such as electric and LH2 systems.