Title :
Design and integration of a solar AMTEC power system with an advanced global positioning satellite
Author :
Johnson, G. ; Hunt, M.E. ; Determan, W.R. ; HoSang, P.A. ; Ivanenok, J. ; Schuller, M.
Author_Institution :
Rockwell Aerosp., Canoga Park, CA, USA
fDate :
2/1/1997 12:00:00 AM
Abstract :
A 1,200-W solar AMTEC (alkali metal thermal-to-electric conversion) power system concept was developed and integrated with an advanced global positioning system (GPS) satellite. The critical integration issues for the SAMTEC with the GPS subsystems included: (1) packaging within the Delta II launch vehicle envelope; (2) deployment and start-up operations for the SAMTEC; (3) SAMTEC operation during all mission phases; (4) satellite field of view restrictions with satellite operations; and (5) effect of the SAMTEC requirements on other satellite subsystems. The SAMTEC power system was compared with a conventional planar solar array/battery power system to assess the differences in system weight, size, and operations, Features of the design include the use of an advanced multitube, vapor anode AMTEC cell design with 24% conversion efficiency, and a direct solar insolation receiver design with integral LiF salt canisters for energy storage to generate power during the maximum solar eclipse cycle, The modular generator design consists of an array of multitube AMTEC cells arranged into a parallel/series electrical network with built-in cell redundancy. Our preliminary assessment indicates that the solar generator design is scaleable over a 500 to 2,500-W range. No battery power is required during the operational phase of the GPS mission. SAMTEC specific power levels greater than 5 We/kg and 160 We/m2 are anticipated for a mission duration of 10 to 12 years in orbits with high natural radiation backgrounds
Keywords :
Global Positioning System; photovoltaic power systems; space vehicle power plants; thermoelectric conversion; 1200 W; 24 percent; Delta II launch vehicle envelope; GPS satellite integration; advanced global positioning satellite; advanced multitube vapor anode AMTEC cell; alkali metal thermal-to-electric conversion; built-in cell redundancy; critical integration issues; deployment; design features; direct solar insolation receiver; field of view restrictions; integral LiF salt canisters; modular generator design; packaging; solar AMTEC power system; solar generator design; start-up operations; Anodes; Batteries; Energy storage; Global Positioning System; Packaging; Power generation; Power systems; Satellites; Solar power generation; Vehicles;
Journal_Title :
Aerospace and Electronic Systems Magazine, IEEE