Session
Weekend Poster Session 1
Location
Utah State University, Logan, UT
Abstract
The PROVES (Pleiades Rapid Orbital Verification Experimental System) Flight Controller Board was irradiated with 200 MeV Protons to a total fluence of 1e10 across multiple runs. Using the n/2000 method [1], this report has concluded the Non-destructive Single Event Effect (SEE) error rate of the Flight Controller Board to be 0.183 SEE per system day.
Proton Single Events Effects Testing by Undergraduate Students for University CubeSat Mission Assurance
Utah State University, Logan, UT
The PROVES (Pleiades Rapid Orbital Verification Experimental System) Flight Controller Board was irradiated with 200 MeV Protons to a total fluence of 1e10 across multiple runs. Using the n/2000 method [1], this report has concluded the Non-destructive Single Event Effect (SEE) error rate of the Flight Controller Board to be 0.183 SEE per system day.
