Title :
Solar thermal power system concepts for high power satellites
Author :
Merrill, John ; Mayberry, Clay S.
Author_Institution :
Adv. Power Group, Air Force Res. Lab., USA
Abstract :
Significant advances in the development of light-weight, compact, reliable, and cost-effective electrical power system (EPS) components are required to enable the design of future large satellite systems (10-100 kWe). Alkali-metal thermal-to-electric converters (AMTEC), a form of direct energy conversion technology, are being developed as a high efficiency, radiation hard converter for high electrical power on a satellite platform. A satellite electrical power system based on AMTEC would consist of a collector to gather sunlight and focus the energy into a receiving cavity surrounded by AMTECs to convert the thermal energy to electrical energy. Large systems are robust and have been projected to achieve specific power levels as high as 14 We/kg in geosynchronous orbits and power levels as high as 150 kWe. An AMTEC based system would accept thermal energy at 1200 K, reject heat at 600 K, and could achieve as high as 25% efficiency with 120 We/kg and 200 We/1 (AMTEC component level) at high voltage (100 V). This paper outlines a conceptual high power solar-thermal system utilizing AMTEC and examines the advantages and disadvantages of such as system as compared to conventional photovoltaic based systems
Keywords :
solar energy concentrators; solar power satellites; space vehicle power plants; thermoelectric conversion; 100 V; 1200 K; 25 percent; AMTEC based system; direct energy conversion; high efficiency; high power satellites; high power solar-thermal system; radiation hard converter; receiver cavity; solar concentrator; solar thermal power system concepts; thermal energy storage; Energy conversion; Orbits; Photovoltaic systems; Power system reliability; Power systems; Robustness; Satellites; Solar heating; Solar power generation; Voltage;
Conference_Titel :
Aerospace Conference Proceedings, 2000 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
0-7803-5846-5
DOI :
10.1109/AERO.2000.878367