NASA's Advanced Radioisotope Power Conversion Technology Development Status

By: Administration (Nasa), National Aeronaut

NASA's Advanced Radioisotope Power Systems (ARPS) project is developing the next generation of radioisotope power conversion technologies that will enable future missions that have requirements that cannot be met by either photovoltaic systems or by current radioisotope power systems (RPSs). Requirements of advanced RPSs include high efficiency and high specific power (watts/kilogram) in order to meet future mission requirements with less radioisotope fuel and lower mass so that these systems can meet requirements for a variety of future space applications, including continual operation surface missions, outer-planetary missions, and solar probe. These advances would enable a factor of 2 to 4 decrease in the amount of fuel required to generate electrical power. Advanced RPS development goals also include long-life, reliability, and scalability. This paper provides an update on the contractual efforts under the Radioisotope Power Conversion Technology (RPCT) NASA Research Announcement (NRA) for research and development of Stirling, thermoelectric, and thermophotovoltaic power conversion technologies. The paper summarizes the current RPCT NRA efforts with a brief description of the effort, a status and/or summary of the contractor's key accomplishments, a discussion of upcoming plans, and a discussion of relevant system-level benefits and implications. The paper also provides a general discussion of the benefits from the development of these advanced power conversion technologies and the eventual payoffs to future missions (discussing system benefits due to overall improvements in efficiency, specific power, etc.). Anderson, David J. and Sankovic, John and Wilt, David and Abelson, Robert D. and Fleurial, Jean-Pierre Glenn Research Center; Jet Propulsion Laboratory NASA/TM-2007-214487, IEEEAC Paper 1610, E-15778 WBS 138494.01.04.01 TECHNOLOGY UTILIZATION; THERMOPHOTOVOLTAIC CONVERSION; RADIOISOTOPE HEAT SOURCES; SPACE MISSIONS; THERMOELECTRICITY; TITAN LAUNCH VEHICLES; CASSINI MISSION; GENERATORS; STIRLING ENGINES; TEMPERATURE DEPENDENCE; X RAY DIFFRACTION; TRANSMISSION ELECTRON MICROSCOPY; THERMAL CONDUCTIVITY

• Format: Paperback
• Language: English
• ISBN: B08DSNCSX2
• ISBN13: 9798670021951
• Release Date: January 1
• Publisher: Independently Published
• Length: 26 Pages
• Weight: 0.19 lbs.
• Dimensions: 0.1" x 8.5"