Asteroid Origins Satellite (AOSAT) I: an On-Orbit Centrifuge Science Laboratory
Asteroid Origins Satellite (AOSAT) I: An On-orbit Centrifuge Science Laboratory Jack Lightholder*, Andrew Thoesen*, Eric Adamson, Jeremy Jakubowski, Ravi Nallapu, Sarah Smallwood, Laksh Raura, Andrew Klesh, Erik Asphaug, Jekan Thangavelautham Arizona State University, Tempe, AZ 85287 Abstract Exploration of asteroids, comets and small moons (`small bodies') can an- swer fundamental questions relating to the formation of the solar system, the availability of resources, and the nature of impact hazards. Near-earth aster- oids and the small moons of Mars are potential targets of human exploration. But as illustrated by recent missions, small body surface exploration remains challenging, expensive, and fraught with risk. Despite their small size, they are among the most extreme planetary environments, with low and irregu- lar gravity, loosely-bound regolith, extreme temperature variation, and the presence of electrically charged dust. Here we describe the Asteroid Origins Satellite (AOSAT-I), an on-orbit, 3U CubeSat centrifuge using a sandwich- sized bed of crushed meteorite fragments to replicate asteroid surface con- ditions. Demonstration of this CubeSat will provide a low-cost pathway to physical asteroid model validation, shed light on the origin and geophysics of asteroids, and constrain the design of future landers, rovers, resource ex- tractors, and human missions. AOSAT-I will conduct scientific experiments within its payload chamber while operating in two distinct modes: 1) as a nonrotating microgravity laboratory to investigate primary accretion, and 2) as a rotating centrifuge producing artificial milligravity to simulate surface conditions on asteroids, comets and small moons. AOSAT-I takes advantage of low-cost, off-the-shelf components, modular design, and the rapid assem- bly and instrumentation of the CubeSat standard, to answer fundamental questions in planetary science and reduce cost and risk of future exploration.
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