Heat Pipe Development For Space Fission Demonstration Missions

Max Chaiken; Marc Andrew Gibson; Jim Sanzi

NASA NTRS · 20210010247

Heat Pipe Development For Space Fission Demonstration Missions

Max Chaiken·Marc Andrew Gibson·Jim Sanzi

Abstract

NASA is currently formulating a flight mission that will demonstrate a 10 kWe nuclear electric fission power system for use on the lunar surface. While preliminary mission concepts leverage the successful Kilopower Reactor Using Stirling Technology ground prototype demonstration of a 1 kWe reactor, there are significant engineering challenges associated with adapting that prototype reactor for flight. One of these challenges is to modify the high temperature sodium heat pipes for use in space operation. Ongoing technical work at the NASA Glenn Research Center seeks to address several key areas of heat pipe development, focusing on fluid return under reduced or microgravity conditions and improved interfaces for both the reactor and the power conversion ends of the heat pipe.

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BibTeX RIS

Max Chaiken, Marc Andrew Gibson, Jim Sanzi. Heat Pipe Development For Space Fission Demonstration Missions. https://ntrs.nasa.gov/citations/20210010247

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