De-orbiting Small Satellites Using Inflatables
Aman Chandra, Jekan Thangavelautham

TL;DR
This paper explores the feasibility of using passive inflatable devices for de-orbiting small satellites, offering a simple alternative to complex propulsion or mechanical systems, especially effective when tumbling.
Contribution
It introduces a passive inflatable de-orbit mechanism that activates during tumbling, providing a potentially simpler and reliable end-of-life solution for small satellites.
Findings
Inflatables can be triggered passively during tumbling.
Inflatable systems are simpler and more robust than mechanical de-orbit devices.
Feasibility analysis shows potential for practical implementation.
Abstract
Small-satellites and CubeSats offer a low-cost pathway to access Low Earth Orbit at altitudes of 450 km and lower thanks to miniaturization and advancement in reliability of commercial electronics. However, at these low altitudes, atmospheric drag has a critical effect on the satellite resulting in natural deorbits within months. As these small systems further increase in reliability and radiation tolerance they will be able readily access higher orbits at altitudes of 700 km and higher, where atmospheric drag has little to no effect. This requires alternative technologies to either de-orbit these small spacecrafts at the end of life or move them to a safe parking orbit. Use of propulsion and de-orbit mechanisms have been proposed, however they require active control systems to be trigged. Other typical de-orbit mechanism relies on complex mechanisms with many moving parts. In this…
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Taxonomy
TopicsSpacecraft Dynamics and Control · Spacecraft Design and Technology · Planetary Science and Exploration
