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The Slirvivable Eower Super Subsystem Demonstration
Electrical Power System Design of High Orbit Satellites
INTEGRATION AND REQUIREMENTS II
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absorption heat pump admittance matrix algorithm analysis application autonomous battery breadboard calculated capability Center charge circuit components condenser configuration cycle detection developed distribution Energy Conversion energy storage Ethernet evaporator expert system fault diagnosis fluid frequency function fuse hardware heat pipe heat pump heat rejection high impedance fault HRSS IECEC IEEE inductor input integrated interface load loop gain lunar monitoring NASA NICBES nuclear operating orbit output panel parameters payload performance Phase photovoltaic power flow power level Power Management power subsystem pressure problem protocol PV system radiator reactor redundant reliability Rocketdyne satellite saturation schedule sensor shown in Figure simulation solar array solar cells solar dynamic Space Power Space Station Freedom spacecraft Stirling Engine subcooling switch SXSS system mass techniques temperature Test Bed Module testbed thermal trickle charge tube voltage