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Digital Techniques in Future Spacecraft Automated Power Systems
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airfoil analysis applications capacity charge circuit collector combustion components condenser configuration conversion cooling cost cycle degradation effect efficiency electrical power electrode electrolyte energy conservation energy storage engine evaluation evaporator flow fluid fuel cell function gas turbine heat exchanger heat pipes heat source heat transfer hot junction hydrogen hydrogen cycle Hydrogen Economy ignition increased input insulation liquid load loss material maximum mission module nuclear operating orbit peak percent performance power plant power subsystem power system pressure production pump radiator range Rankine Cycle ratio reduced regulator shown in Figure shunt silicon solar array solar cell solar energy solar power space spacecraft specific stack Stirling engine surface Table temperature thermal battery thermoelectric tion transport unit utility valve vent voltage volts waste heat watts weight welding