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Thermal analyses of heat source assembly for a dual loop, Turbo-Brayton Radioisotope power system

  • Published:2019-05 Issue: Volume:10 Page:82-91
  • ISSN:2451-9049
  • Container-title:Thermal Science and Engineering Progress
  • language:en
  • Short-container-title:Thermal Science and Engineering Progress

Author:

El-Genk Mohamed S.,Schriener Timothy M.,Breedlove Jeffrey J.

Funder

Office of Nuclear Energy

U.S. Department of Energy

National Aeronautics and Space Administration

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes

Reference38 articles.

1. Space Nuclear Power;Angelo,1985

2. Design of Multihundredwatt DIPS for robotic space missions;Bents,1991

3. Turbo-Brayton converter for radioisotope power systems;Breedlove,2018

4. Development of Advanced Stirling Radioisotope Generator for Space Exploration, NASA Technical Report NASA/TM-2007-214806;Chan,2007

5. A Performance comparison of SiGe and Skutterudite Basd segmented thermoelectric devices;El-Genk,2002
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