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Highly-miniaturized spacecraft "PlanarSat": Evaluating prospects and challenges through a survey of femto & atto satellite missions

dc.contributor.authorUludag, Mehmet Sevket
dc.contributor.authorAslan, Alim Rustem
dc.contributor.orcid0000-0003-0432-0389
dc.contributor.researcheridLXV-4628-2024
dc.contributor.researcheridN-9250-2013
dc.date.accessioned2025-10-21T09:39:02Z
dc.date.issued2025-07-10
dc.description.abstractAs satellite technology advances, there has been a notable trend towards miniaturization, leading to the development of increasingly smaller satellites such as femtosatellites and attosatellites. A new emerging form of such satellites is often called ChipSat, with unique designs that utilize both surfaces of a single plane to maximize functionality within limited dimensions. Initially, the term ChipSat referred to system-on-a-chip satellites but it has since expanded to include centimeter and millimeter scale spacecraft. To provide a clearer terminology, this paper introduces the term "PlanarSat" for such a planar spacecraft. Despite the challenges in deployment and the constraints, such as cost, size, access to space, and capabilities, of miniaturized subsystems, these satellites represent a significant shift in space technology, aiming for costeffective solutions and innovative mission capabilities. This study reviews thirty sub-100-gram satellites, analyzing their design, deployment, and potential for future advancements in a comparative manner. In this study, satellite independence was defined based on system-wise independence, highlighting operational autonomy irrespective of physical connections. The survey's findings highlight technological advancements and potential applications for these very small spacecraft, which are pushing the boundaries of what is feasible with smaller satellites and how these satellites were or planned to be delivered to orbit. The analysis results provide a basic cost comparison, providing information on hardware and launch costs, taking the instantaneous data rate as a reference point, underscoring the need for a new systems engineering approach to the design of such satellites.
dc.identifier.doi10.1016/j.actaastro.2025.05.018
dc.identifier.endpage358
dc.identifier.issn0094-5765
dc.identifier.startpage343
dc.identifier.urihttps://hdl.handle.net/11452/56123
dc.identifier.volume236
dc.identifier.wos001536830600001
dc.indexed.wosWOS.SCI
dc.language.isoen
dc.publisherPERGAMON-ELSEVIER SCIENCE LTD
dc.relation.journalACTA ASTRONAUTICA
dc.subjectDESIGN
dc.subjectFEMTOSATELLITE
dc.subjectDECAY
dc.subjectFemtosatellite
dc.subjectAttosatellite
dc.subjectMiniaturization
dc.subjectSmall spacecraft
dc.subjectChipsat
dc.subjectPlanarsat
dc.subjectPCBSat
dc.subjectScience & Technology
dc.subjectTechnology
dc.subjectEngineering, Aerospace
dc.subjectEngineering
dc.titleHighly-miniaturized spacecraft "PlanarSat": Evaluating prospects and challenges through a survey of femto & atto satellite missions
dc.typeArticle
dspace.entity.typePublication
local.indexed.atWOS

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