TY - GEN
T1 - Carbon-carbon-composite salt-cooled electric space reactors
AU - Forsberg, C. W.
AU - Burchell, T. D.
AU - Williams, D. F.
AU - Holcomb, D. E.
AU - Holdaway, R. F.
AU - Qualls, A. L.
PY - 2005
Y1 - 2005
N2 - The primary requirements for a deep space or planetary nuclear reactor for production of electricity are reliability, long life, and a high power-to-mass ratio. Advanced reactors (core, structure, power-conversion systems, radiator, etc.) are proposed that are built entirely from carbon-based materials that use salts (liquid or gas) as the heat transfer medium between the reactor and power-generation equipment and/or heat rejection systems to create reactor systems with very high power-to-mass ratios. While currently proposed space nuclear reactors have peak temperatures between 900 and 1400K with potential efficiencies as high as 30% for advanced Stirling engines, the new reactors would have peak operating temperatures between 1800 and 2300K with potential efficiencies twice that of other concepts. Because there are no other classes of materials that can potentially operate at such temperatures and have very low masses, most of the components of such a space electric nuclear reactor must be built of carbon-based materials. Based on theoretical considerations and the developments in carbon-carbon technologies over the last 20 years, such machines appear to be potentially viable. However, significant research is required to demonstrate feasibility and a major long-term development program would be required to build such machines.
AB - The primary requirements for a deep space or planetary nuclear reactor for production of electricity are reliability, long life, and a high power-to-mass ratio. Advanced reactors (core, structure, power-conversion systems, radiator, etc.) are proposed that are built entirely from carbon-based materials that use salts (liquid or gas) as the heat transfer medium between the reactor and power-generation equipment and/or heat rejection systems to create reactor systems with very high power-to-mass ratios. While currently proposed space nuclear reactors have peak temperatures between 900 and 1400K with potential efficiencies as high as 30% for advanced Stirling engines, the new reactors would have peak operating temperatures between 1800 and 2300K with potential efficiencies twice that of other concepts. Because there are no other classes of materials that can potentially operate at such temperatures and have very low masses, most of the components of such a space electric nuclear reactor must be built of carbon-based materials. Based on theoretical considerations and the developments in carbon-carbon technologies over the last 20 years, such machines appear to be potentially viable. However, significant research is required to demonstrate feasibility and a major long-term development program would be required to build such machines.
UR - https://www.scopus.com/pages/publications/27844450959
M3 - Conference contribution
AN - SCOPUS:27844450959
SN - 0894486969
SN - 9780894486968
T3 - American Nuclear Society Embedded Topical Meeting - 2005 Space Nuclear Conference
SP - 54
EP - 61
BT - American Nuclear Society Embedded Topical Meeting - 2005 Space Nuclear Conference
T2 - American Nuclear Society Embedded Topical Meeting - 2005 Space Nuclear Conference
Y2 - 5 June 2005 through 9 June 2005
ER -