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A scientific study of the problems of digital engineering for space flight systems,
with a view to their practical solution.


1998 Military and Aerospace Applications of

Programmable Devices and Technologies Conference

(MAPLD Conference)

 

PCD8: S. Shanken, J. Patterson, J. Parkinson, D. Czajkowski
Space Electronics Inc.

"Reprogrammable, Non-Volatile EEPROM Multi-Chip Module (MCM) for Radiation-Hardened Space Applications"

PCD8_Strobel.pdf

PCD8_Strobel.doc

A high density (8 megabit) multi-chip module (MCM) has been developed for space applications. This MCM combines commercial-off-the-shelf (COTS) silicon and Space Electronics’ Rad-PakÒ technology. The design approach and resulting electrical performance is outlined. Wafer/Die Lot acceptance of COTS die will be presented, including SEM analysis of metalization.  Both total ionizing does (TID) and single event effects (SEE) data are presented. Radiation tolerance in several NASA mission orbits is calculated using Space Radiation 4.0.


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