PEDRO-V: From a concurrent engineering case study to a promising phase zero mission definition
Domenico D'Auria, Arianna Rigo, Luca Niero, Andrei-Toma Stoica, Vito, Costantini, Pasquale Castellano, Zsofia Zita Szilagyi, Nishani Vijayakumaran,, Ella Toppari, Stefano Schiano, Marco Adorno, Matteo Matrone, Chiara Tulli,, Jan Kurowski, Leo Bougault, Argenziano Francesco

TL;DR
This paper presents a case study of ESA's student challenge where concurrent engineering methods enabled rapid, effective space mission design, culminating in the PEDRO-V Venus mission proposal.
Contribution
It demonstrates the successful application of concurrent engineering in an academic setting for space mission concept development and feasibility assessment.
Findings
Concurrent engineering enabled rapid design convergence.
Student teams effectively defined mission subsystems and requirements.
The PEDRO-V mission feasibility was successfully confirmed.
Abstract
Each year, the European Space Agency (ESA) organizes challenges for university students, from BSc to PhD levels. The ESA Concurrent Engineering Challange 2024 was hosted by four Concurrent Design Facilites (CDF) across Europe: ESEC Galazia, ISAE SUPAERO, the University of Athens, and the University of Portsmouth. A total of 102 students participated in the event. Over five days, students worked on a feasibility study for a space mission, simulating ESA's design session at ESTEC, the ESA headquarters. Students were divided into specializes groups based on their backgrounds, reflecting ESA's concurrent engineering teams. This paper discusses the design of subsystems by students, their trade-off results, and the outcomes of the CDF study. It highlights the effectiveness of concurrent engineering, which enabled rapid and efficient results even from non-esxpert teams. The future development…
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Taxonomy
TopicsSpacecraft Design and Technology · Rocket and propulsion systems research · Spacecraft and Cryogenic Technologies
