U.S. Department of EnergyOffice of Scientific and Technical Information
A Gas-Cooled Reactor Surface Power System
Abstract
A human outpost on Mars requires plentiful power to assure survival of the astronauts. Anywhere from 50 to 500 kW of electric power (kWe) will be needed, depending on the number of astronauts, level of scientific activity, and life-cycle closure desired. This paper describes a 250-kWe power system based on a gas-cooled nuclear reactor with a recuperated closed Brayton cycle conversion system. The design draws upon the extensive data and engineering experience developed under the various high-temperature gas cooled reactor programs and under the SP-100 program. The reactor core is similar in power and size to the research reactors found on numerous university campuses. The fuel is uranium nitride clad in Nb1%Zr, which has been extensively tested under the SP-I 00 program. The fuel rods are arranged in a hexagonal array within a BeO block. The BeO softens the spectrum, allowing better use of the fuel and stabilizing the geometry against deformation during impact or other loadings. The system has a negative temperature feedback coefficient so that the power level will automatically follow a variable load without the need for continuous adjustment of control elements. Waste heat is removed by an air-cooled heat exchanger using cold Martian air. The amountmore »
- Authors:
-
- Sandia National Laboratories (SNL-NM), Albuquerque, NM (United States)
- Publication Date:
- Research Org.:
- Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
- Sponsoring Org.:
- USDOE National Nuclear Security Administration (NNSA), Nuclear Criticality Safety Program (NCSP)
- OSTI Identifier:
- 1637
- Report Number(s):
- SAND98-2494C
Journal ID: ISSN 0094-243X; ON: DE00001637
- DOE Contract Number:
- AC04-94AL85000
- Resource Type:
- Conference
- Journal Name:
- AIP Conference Proceedings
- Additional Journal Information:
- Journal Volume: 458; Conference: 1999 Space Technology and Applications International Forum, Albuquerque, NM (United States), 31 Jan - 4 Feb 1999; Journal ID: ISSN 0094-243X
- Publisher:
- American Institute of Physics (AIP)
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 21 SPECIFIC NUCLEAR REACTORS AND ASSOCIATED PLANTS; Mars Planet; HTGR Type Reactors; Brayton Cycle; Power Range 10-100 kW; Nuclear Criticality Safety Program (NCSP); NESDPS Office of Nuclear Energy Space and Defense Power Systems; Light Water Reactor (LWR); Electric Power (kWe); Fuel Rods; Reactor Technology; Brayton System; Turbomachinery; Recuperator; Heat Rejection Unit; Radiation Shield
Citation Formats
Lipinski, Ronald J., Wright, Steven A., Lenard, Roger X., and Harms, Gary A. A Gas-Cooled Reactor Surface Power System. United States: N. p., 1999.
Web. doi:10.1063/1.57544.
Lipinski, Ronald J., Wright, Steven A., Lenard, Roger X., & Harms, Gary A. A Gas-Cooled Reactor Surface Power System. United States. https://doi.org/10.1063/1.57544
Lipinski, Ronald J., Wright, Steven A., Lenard, Roger X., and Harms, Gary A. 1999.
"A Gas-Cooled Reactor Surface Power System". United States. https://doi.org/10.1063/1.57544. https://www.osti.gov/servlets/purl/1637.
@article{osti_1637,
title = {A Gas-Cooled Reactor Surface Power System},
author = {Lipinski, Ronald J. and Wright, Steven A. and Lenard, Roger X. and Harms, Gary A.},
abstractNote = {A human outpost on Mars requires plentiful power to assure survival of the astronauts. Anywhere from 50 to 500 kW of electric power (kWe) will be needed, depending on the number of astronauts, level of scientific activity, and life-cycle closure desired. This paper describes a 250-kWe power system based on a gas-cooled nuclear reactor with a recuperated closed Brayton cycle conversion system. The design draws upon the extensive data and engineering experience developed under the various high-temperature gas cooled reactor programs and under the SP-100 program. The reactor core is similar in power and size to the research reactors found on numerous university campuses. The fuel is uranium nitride clad in Nb1%Zr, which has been extensively tested under the SP-I 00 program. The fuel rods are arranged in a hexagonal array within a BeO block. The BeO softens the spectrum, allowing better use of the fuel and stabilizing the geometry against deformation during impact or other loadings. The system has a negative temperature feedback coefficient so that the power level will automatically follow a variable load without the need for continuous adjustment of control elements. Waste heat is removed by an air-cooled heat exchanger using cold Martian air. The amount of radioactivity in the reactor at launch is very small (less than a Curie, and about equal to a truckload of uranium ore). The system will need to be engineered so that criticality cannot occur for any launch accident. This system is also adaptable for electric propulsion or life-support during transit to and from Mars.},
doi = {10.1063/1.57544},
url = {https://www.osti.gov/biblio/1637},
journal = {AIP Conference Proceedings},
issn = {0094-243X},
number = ,
volume = 458,
place = {United States},
year = {Sun Jan 31 00:00:00 EST 1999},
month = {Sun Jan 31 00:00:00 EST 1999}
}