Proton-Induced Single Event Upsets in 71 Earth-Satellite Environments.
NAVAL RESEARCH LAB WASHINGTON DC
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Predicted upset rates are presented, as a function of one experimental parameter, for devices in small earth satellites. Contour maps of SEU rate versus circular orbit inclination and altitude allow predictions at 180-1400 km and 27 deg to 90 deg. A computer program is listed, permitting the reader to calculate upsets in any proton flux. Author
- Computer Programming and Software
- Computer Hardware
- Spacecraft Trajectories and Reentry