Hello there analog community,
We are developing payloads for space missions and we have some important doubts regarding part AD8629/AD8629S
which we need to be resolved to ensure the functionality of our designs.
The main doubt is related with the space model AD8629S in which the Bias Current seems to be much bigger than those in the commercial model.
In the commercial datasheet the bias currents are 30pA (typical) to 100pA (max) and shows a graph (Input Bias Current vs Input Common-Mode Voltage for several temperatures) which imply that the bias current could be 10pA for Vcm = 0.5V (e.g) and 25ºC (and much less for even lower temperatures! which is good for us).
The space part datasheet (http://www.analog.com/media/en/technical-documentation/data-sheets/AD8629S.pdf ) tells bias current limits are -500pA (min) to 500pA (max) but it doesn’t say which are the typical values or at least
the variation of this bias current VS Temperature (similar to those in the commercial datasheet).
So, why is such a change between bias current values from space part AD8629S to commercial part AD8629? What are the typical values for this parameter in the space model?
Some Op Amps whose commercial part has pA as Ibias says to not use a compensating resistance in a transimpedance configuration because the bias current is already compensated internally (so adding this R will do things worse). Can we use a compensating resistance to cancel the effect of Ibias in AD8629S?
I hope you can shed some light on this... Thank you very much in advance.