Design for Spacecraft Reuse: A Systems Perspective on Circularity in Space
2026 (English)Doctoral thesis, comprehensive summary (Other academic)Alternative title
Design för återanvändning av rymdfarkoster: Ett systemperspektiv på cirkularitet i rymden (Swedish)
Abstract [en]
Declining launch costs and accelerating innovation cycles are driving the rapid expansion of the space industry. While space technologies deliver significant societal and economic benefits, this growth exposes the limitations of a single-use paradigm in spacecraft design. Safe and sustainable space operations are threatened by escalating environmental degradation and the proliferation of orbital debris. Implementing Circular Economy (CE) practices offers a promising pathway to address these threats, yet efforts in the space industry remain fragmented and lack systemic coordination. With a predominant focus on reusable launch vehicles, emerging satellite reuse remains limited.
To address this, this thesis advances Design-for-Spacecraft-Reuse (DfSR), a design concept for embedding circularity in space systems, with satellites as its primary application context within the broader spacecraft category. Methodologically, this research employs a qualitative, abductive approach grounded in systems thinking, socio-technical transition theory, and engineering design theory. The empirical foundation draws on expert interviews and case studies. Literature reviews provide theoretical and contextual framing.
A central finding is that satellite reuse pathways are orbit-conditioned: distinct orbital regimes imply distinct reuse logics, each with its own design and system-level implications. The findings further reveal that the predominant focus on isolated technical solutions, such as reusable launch vehicles, can contribute to fragmentation and limit the implementation of CE practices in the space industry. Across the findings, design emerges as the layer integrating orbital context and system-level conditions, operationalized through DfSR.
The contributions are threefold: (1) Empirical insights into the factors driving fragmentation of CE practices in the space industry and their implications for coordinated implementation. (2) A systems-perspective analysis of how CE conditions shape satellite reuse across system levels. (3) Design support artifacts that operationalize DfSR for satellite reuse, including a conceptual regime-differentiated design framework linking orbital context to design requirements, and a set of design considerations bridging system-level conditions and early-stage satellite design practices. Together, and through DfSR, the contributions of this thesis provide a basis to embed circularity and establish reuse as a design principle in satellite development, supporting the industry transition toward circularity in space. While focused on satellites, the contributions offer transferable insights across the spacecraft category.
Place, publisher, year, edition, pages
Luleå, Sweden: Luleå University of Technology, 2026.
Series
Doctoral thesis / Luleå University of Technology, ISSN 1402-1544
Keywords [en]
Satellite Reusability, Circular Space Economy, Circular Systems, Circular Design, Engineering Design, Design-for-Spacecraft-Reuse, Space Sustainability, Orbital Regimes, Operational Regimes, Industrial Transformation
National Category
Vehicle and Aerospace Engineering
Research subject
Product Innovation
Identifiers
URN: urn:nbn:se:ltu:diva-117276ISBN: 978-91-8142-065-4 (print)ISBN: 978-91-8142-066-1 (electronic)OAI: oai:DiVA.org:ltu-117276DiVA, id: diva2:2055897
Public defence
2026-06-17, C305, Luleå University of Technology, Luleå, 09:00 (English)
Opponent
Supervisors
Projects
Creaternity Aerospace Lab2026-04-272026-04-272026-05-12Bibliographically approved
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