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1

Wilson, David Gordon. High-efficiency Brayton-cycle engines for marine propulsion. Alton: Microinfo, 1985.

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2

Garrett Turbine Engine Company. Engineering Staff and United States. National Aeronautics and Space Administration, eds. Brayton cycle solarized advanced gas turbine: Final report. [Washington, DC: National Aeronautics and Space Administration, 1986.

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3

Wilson, David Gordon. High-efficiency Brayton-cycle engines for marine propulsion. Cambridge, Mass: Massachusetts Institute of Technology, Sea Grant College Program, 1985.

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4

Wilson, David Gordon. High-efficiency Brayton-cycle engines for marine propulsion. Cambridge, Mass: Massachusetts Institute of Technology, Sea Grant College Program, 1985.

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5

Backman, Jari. On the reversed Brayton cycle with high speed machinery / Jari Backman. Lappeenranta, Finland: Lappeenranta University of Technology, 1996.

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6

English, Robert E. Technology for Brayton-cycle space powerplants using solar and nuclear energy. Cleveland, Ohio: Lewis Research Center, 1986.

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7

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Technology for Brayton-cycle space powerplants using solar and nuclear energy. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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8

Mason, Lee S. A comparison of Brayton and Stirling space nuclear power systems for power levels from 1 kilowatt to 10 megawatts. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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9

Lantz, Richard Daryl. Design study of a modular gas-cooled, closed-Brayton cycle reactor for marine use. Springfield, Va: Available from the National Technical Information Service, 1989.

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10

Shaltens, Richard K. 800 hours of operational experience from a 2 kW[subscript e] solar dynamic system. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.

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11

W, Carlson Albert, and United States. National Aeronautics and Space Administration., eds. Solar dynamic heat rejection technology: Task 1 : system concept development, final report. [Washington, DC]: National Aeronautics and Space Administration, 1987.

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12

Ma, Zhiwen. Advanced supercritical carbon dioxide power cycle configurations for use in concentrating solar power systems: Preprint. Golden, CO]: National Renewable Energy Laboratory, 2011.

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13

S, El-Genk Mohamed, Harper William B, and United States. National Aeronautics and Space Administration., eds. Closed Brayton cycle power system with a high temperature pellet bed reactor heat source for NEP applications. [Washington, DC: National Aeronautics and Space Administration, 1993.

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14

Center, Langley Research, ed. High-speed engine/component performance assessment using exergy and thrust-based methods. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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15

Center, Langley Research, ed. High-speed engine/component performance assessment using exergy and thrust-based methods. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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16

S, Bloomfield Harvey, and United States. National Aeronautics and Space Administration., eds. Development of lightweight radiators for lunar based power systems. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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17

United States. National Aeronautics and Space Administration., ed. Preliminary design for a reverse Brayton cycle cryogenic cooler: Phase I final report, period of performance, September 1990-December 1992. Hanover, NH: Creare, Inc., 1993.

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18

A, Hall Carsie, and Lewis Research Center, eds. Thermal state-of-charge in solar heat receivers. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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19

Alexander, Dennis. 2 kWe Solar Dynamic Ground Test Demonstration Project. [Washington, DC]: National Aeronautics and Space Administration, 1997.

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20

Alexander, Dennis. 2 kWe Solar Dynamic Ground Test Demonstration Project. [Washington, DC]: National Aeronautics and Space Administration, 1997.

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21

Alexander, Dennis. 2 kWe Solar Dynamic Ground Test Demonstration Project. [Washington, DC]: National Aeronautics and Space Administration, 1997.

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22

W, Culver Donald, Bulman Melvin J, and United States. National Aeronautics and Space Administration., eds. Human exploration and settlement of the moon using LUNOX-augmented NTR propulsion. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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23

Christopher, Krystkowiak, Klucher Beth A, and United States. National Aeronautics and Space Administration., eds. Design of the heat receiver for the U.S./Russia solar dynamic power joint flight demonstration. [Washington, DC: National Aeronautics and Space Administration, 1996.

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24

Christopher, Krystkowiak, Klucher Beth A, and United States. National Aeronautics and Space Administration., eds. Design of the heat receiver for the U.S./Russia solar dynamic power joint flight demonstration. [Washington, DC: National Aeronautics and Space Administration, 1996.

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25

United States. National Aeronautics and Space Administration., ed. Improved boundary layer heat transfer calculations near a stagnation point: Final report. Cleveland, Ohio: Cleveland State University, 1990.

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26

B, Ibrahim Mounir, and United States. National Aeronautics and Space Administration., eds. Analysis of thermal energy storage material with change-of-phase volumetric effects. [Washington, D.C: National Aeronautics and Space Administration, 1990.

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27

Cain, W. G. Heat exchanger development for steam injected Brayton Cycle. Mechanical Technology Incorporated, 1988.

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28

Technology for Brayton-cycle space powerplants using solar and nuclear energy. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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29

National Aeronautics and Space Administration (NASA) Staff. Evaluation of a Brayton Cycle Recuperator after 21,000 Hours of Ground Testing. Independently Published, 2018.

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30

National Aeronautics and Space Administration (NASA) Staff. Conceptual Design Study of a Closed Brayton Cycle Turbogenerator for Space Power Thermal-To-Electric Conversion System. Independently Published, 2018.

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31

High-speed engine/component performance assessment using exergy and thrust-based methods. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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32

Rez, Peter. Electrical Power Generation: Fossil Fuels. Oxford University Press, 2017. http://dx.doi.org/10.1093/oso/9780198802297.003.0004.

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Nearly all electrical power is generated by rotating a coil in a magnetic field. In most cases, the coil is turned by a steam turbine operating according to the Rankine cycle. Water is boiled and heated to make high-pressure steam, which drives the turbine. The thermal efficiency is about 30–35%, and is limited by the highest steam temperature tolerated by the turbine blades. Alternatively, a gas turbine operating according to the Brayton cycle can be used. Much higher turbine inlet temperatures are possible, and the thermal efficiency is higher, typically 40%. Combined cycle generation, in which the hot exhaust from a gas turbine drives a Rankine cycle, can achieve thermal efficiencies of almost 60%. Substitution of coal-fired by combined cycle natural gas power plants can result in significant reductions in CO2 emissions.
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33

Early results from solar dynamic space power system testing. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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34

Sydnor, Katherine Anne. Design features of small Brayton cycles for autonomous underwater vehicles. 1987.

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