I. Introduction
Optocouplers are simple devices compared to conventional integrated circuits, but they have proven to be somewhat difficult to use in space because they require high internal gain to amplify photocurrent produced by internal light-emitting diodes (LEDs) (net power transfer from the LED to the photodetector is on the order of 0.1%). Space failures have occurred from two different mechanisms: displacement damage from high-energy protons, which produces Properties of the Optocouplers Used in the Study
Device | Manu- facturer | Input Current (mA) | Current Transfer Ratio | LED Technology |
---|---|---|---|---|
6N139 | Agilent | 0.5 | 20 | Double-Het |
HCPL4701 | Agilent | 0.04 | 35 | Double-Het |
HCNR200 | Agilent | 0.1–10 | 0.005* | Double-Het. |
4N49 | Micropac | 1 | 2 | Amphoteric |
*The HCNR200 contains no active gain elements. The current transfer ratio is the ratio between current in either of the two photodiodes to the forward current of the LED. |