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Energy Storage System Needs for Future Planetary Missions • Primary Batteries/Fuel Cells for Surface Probes: High Temperature Operation (> 465C) High Specific Energy (>400 Wh/kg) Operation in Corrosive Environments • Rechargeable Batteries for Aerial Platforms: High Temperature Operation (300-465C) Operation in Corrosive Environments Low-Medium Cycle Life High Specific Energy (>200 Wh/kg) Operation in High Pressures • Primary Batteries/Fuel cells for planetary landers/probes: High Specific Energy (> 500 Wh/kg), Long Life (> 15 years), Radiation Tolerance & Sterilizable by heat or radiation Icy Giants Inner Planets Outer Planets • Rechargeable Batteries for flyby/orbital missions: High Specific Energy (> 250 Wh/kg) Long Life (> 15 years) Radiation Tolerance & Sterilizable by heat or radiation. • Low temperature Batteries for Probes and Landers: Low Temperature Primary batteries (< -80C) Low Temperature Rechargeable Batteries (< -60 C) Europa Orbiter Uranus/Neptune missions All images are Artist’s Concepts Europa Lander 10PDF Image | NASA Fuel Cell and Hydrogen Activities
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