Optimizing Systems Engineering Procedure for the Development of a Sounding Rocket
摘要
Rocket development’s multidisciplinary nature necessitates systems engineering methodologies, but the breadth of knowledge required can challenge novice students. The Space Launch Vehicle and Space Transportation (SLV∙ST) project aims to address this by developing a two-stage sounding rocket with a novel propulsion system, the Rotating Detonation Rocket Engine (RDRE), under student researchers’ guidance. This initiative seeks to cultivate specialized talent and strengthen aerospace infrastructure, including essential ground systems for mission monitoring. To make systems engineering more accessible, we are adapting established frameworks for small-scale rocket projects. By customizing the System Design Process (SDP) and Technical Management Process (TMP), the project provides a more pragmatic approach to rocket development, offering valuable insights for student researchers. These methods are expected to aid in understanding and applying systems engineering concepts within aerospace and related fields.