by Jack Shue, NASA GSFC Code 563 , Organizational website, Jun 22 2010
Focus:
A more complete title for this 24-slide presentation might be “Power Electronics for the
Next Gen of Space Power Systems.†A key theme here is the challenge of satisfying supply
voltage requirements for on-board logic in light of battery voltage variations and voltage
drops in a distributed power architecture. Related to that, is the impact of FPGAs, which
are demanding that switching regulators be applied at the point of load. It begins with a
discussion of battery issues, comparing weight, energy density and voltage variation for
different chemistries used in space followed by discussion of allowable supply voltage
variations for the range of electronics logic used in space; top 5 problems in developing
space power systems; and power distribution issues. A power system case study is briefly
described including the attempts to power multiple FPGAs using LDOs, homemade linear
regulators, and ultimately, standard linear regulators. A problem with MOSFET—induced
thermal instability experienced in design of the homemade linear regulator is discussed.
Presentation concludes by explaining the need for a switching regulator at the point of
load, status of these parts and plans to qualify and test them for space.
What you’ll learn:
Notes:
Following the publication of this presentation, several commercial, point-of-load
switching regulators were introduced for space. To read about them see "Rad-Hard Power
Converters Ride Intermediate Bus Into Space" in the August 2011 issue of How2Power Today,
http://www.how2power.com/newsletters/1208/products/H2PToday1208_products_SpacePowerReport.
pdf.
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