Finite element analysis of plasma flows in cusped discharge chambers

Abstract

Fig. 3 Mass vs time for various array orientation options for station in 500-km orbit. Jackson, L. R., Moses, P. L., Scotti, S. J., and Blosser, M. L., Operational Modules for Station Construction, NASA TM 85772, April 1984. Baraona, C. R., Space Station Power System, Photovoltaic Research and Technology, NASA CP 2475, 1986, pp. 321-332. Rockwell International, Power System Description Document, NASA Lewis Research Center, DR:SE-02, Sept. 11, 1987. Bilardo, V., Jr., and Hudiburg, J., An Assessment of Nominal and Contingency Altitude Reboost Scenarios During Station Assembly, AIAA Paper 88-2638, June 1988. Lillington, D. R., Kukulka, J. R., Mason, A. V., Sater, B., and Sanchez, J., Optimization of Silicon 8cm x 8cm Wrapthrough Station Cells for On Orbit Operation, 20th IEEE Photovoltaic Specialists Conference, Institute of Electrical and Electronics Engineers, York, Sept. 1988, pp. 934-939. Hough, W. W., and Elrod, B. D., Solar Array Performance as a Function of Orbital Parameters and Spacecraft Attitude, Transactions of the ASME, Journal of Engineering for Industry, Vol. 91, Feb. 1969, pp. 13-20. Jacchia, L. G., New Static Models of the Thermosphere and Exosphere with Empirical Temperature Profiles, Smithsonian Astrophysteal Observatory Special Report, No. 313; also NASA CR-112684, 1970.