|Name||Armadillo (Attitude Related Maneuvers And Debris Instrument in Low (L) Orbit)|
|Units or mass||3U|
|Status||Reentry 2022-08-23. Was operational (Beaconed but ground station software issues delayed commanding to January 2022 as per SmallSat 2022 paper)|
|Deployer||P-POD (Poly-Picosatellite Orbital Deployer)|
|Organisation||University of Texas|
|Entity||Academic / Education|
Characterize in-situ sub-millimeter level dust and debris particles in LEO.
Characterize in-situ sub-millimeter level dust and debris particles in LEO by sensing impacts at varying times, directions and locations. Demonstrate ionospheric radio-occultation within a single CubeSat volume (10 cm x 10 cm x 10 cm) using a software-defined dual frequency GPS receiver. Train students in best systems engineering practices by executing a complete spacecraft life cycle from concept design to mission operations. Precise attitude control for nanosatellites, a cold-gas micropropulsion system and a miniaturized dust/debris detector.
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