Concept of a Green Propulsion System for Ioshex, Designed to Perform In-Orbit Randezvous and Docking

Recent challenges in space access include cost optimization and space debris reduction. The European Space Agency has envisioned the evolution of in-orbit transportation involving re-usable service vehicles, moving payloads from high parking orbits to their target orbits. This concept for orbital in...

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Bibliographic Details
Published in:Transactions on aerospace research 2024-09, Vol.2024 (3), p.58-76
Main Authors: Surmacz, Paweł, Parzybut, Adrian, Gramatyka, Jakub, Bodych, Daria, Rugor, Łucja, Uwarowa, Inna, Mariani, Marco, Guerzoni, Marco
Format: Article
Language:English
Subjects:
chemical propulsion
docking
hydrogen peroxide
orbital infrastructure
rendezvous
servicing spacecraft
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Summary:Recent challenges in space access include cost optimization and space debris reduction. The European Space Agency has envisioned the evolution of in-orbit transportation involving re-usable service vehicles, moving payloads from high parking orbits to their target orbits. This concept for orbital infrastructure requires de-risking activities and the development of building blocks, such as standardized interfaces and communication. Mastery of close-proximity operations and docking is essential for the new transportation system. This new branch of space operations represents a good opportunity to introduce more sustainable propulsion solutions, especially given the high costs and uncertain future of hydrazine and its derivatives. IOSHEX, a service spacecraft to be equipped with a green propulsion system utilizing 98% hydrogen peroxide, serves as a reference. This paper presents a design concept for this propulsion system, including trade-off analyses, calculations, and a three-dimensional model integrated with IOSHEX.
ISSN:2545-2835
2545-2835
DOI:10.2478/tar-2024-0016