Power considerations for long duration balloon flights |
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| Institution: | 1. Physics Department, Case Western Reserve University, Cleveland, OH 44106, U.S.A.;7. Space Science Laboratory, The Aerospace Corporation, El Segundo, CA 90245, U.S.A.;71. R.A.A.F. Physics Department, Melbourne University, Parkville, Victoria, Australia;1. Department of General Education, Faculty of Science and Technology, Meijo University, 1-501, Shiogamaguchi, Tempaku-ku, Nagoya, 468-8502, Japan;2. Institute for Materials Research, Tohoku University, 2-1-1, Katahira, Sendai, 980-8577, Japan;3. NGK SPARK PLUG Co., LTD, Nagoya, Japan;4. Institute Radioscience Research Laboratory, Faculty of Science, Shizuoka University, Shizuoka, 816-8580, Japan;5. Department of Research, Nagoya Industrial Research Institute, Noa Yotsuya Bld. 2F, 1-13, Yotsuya-tori, Chikusa-ku, Nagoya, 464-8019, Japan;1. Centre for Research in Earth and Space Science, York University, 4700 Keele Street Toronto, M3J1P3, ON, Canada;2. NASA Jet Propulsion Laboratory, 4800 Oak Grove Dr, Pasadena, CA91109, USA;3. NASA Goddard Space Flight Centre, 8800 Greenbelt Rd, Greenbelt, MD, 20771, USA |
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| Abstract: | A solar panel, silicad battery power supply system is described which provided 100 W of power for a balloon borne solar neutron experiment. The system operated successfully on a 22 day circum-global RACOON flight launched from Australia in January 1983. |
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