Journal articles on the topic 'Space Radioisotope Power Systems'

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1

Yang, Jihui, and Thierry Caillat. "Thermoelectric Materials for Space and Automotive Power Generation." MRS Bulletin 31, no. 3 (March 2006): 224–29. http://dx.doi.org/10.1557/mrs2006.49.

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AbstractHistorically, thermoelectric technology has only occupied niche areas, such as the radioisotope thermoelectric generators for NASA's spacecrafts, where the low cooling coefficient of performance (COP) and energy-conversion efficiency are outweighed by the application requirements.Recent materials advances and an increasing awareness of energy and environmental conservation issues have rekindled prospects for automotive and other applications of thermoelectric materials.This article reviews thermoelectric energy-conversion technology for radioisotope space power systems and several proposed applications of thermoelectric waste-heat recovery devices in the automotive industry.
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2

Mason, Lee S. "Realistic Specific Power Expectations for Advanced Radioisotope Power Systems." Journal of Propulsion and Power 23, no. 5 (September 2007): 1075–79. http://dx.doi.org/10.2514/1.26444.

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3

Kramer, Daniel P., Richard Ambrosi, Mark Sarsfield, Emily Jane Watkinson, Ramy Mesalam, Hugo Williams, Chadwick Barklay, et al. "Recent Joint Studies Related to the Development of Space Radioisotope Power Systems." E3S Web of Conferences 16 (2017): 05002. http://dx.doi.org/10.1051/e3sconf/20171605002.

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4

Hunt, M. E. "High efficiency dynamic radioisotope power systems for space exploration-a status report." IEEE Aerospace and Electronic Systems Magazine 8, no. 12 (December 1993): 18–23. http://dx.doi.org/10.1109/62.246037.

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5

Watkinson, Emily Jane, Ramy Mesalam, Jean-François Vigier, Ondřej Beneš, Jean-Christophe Griveau, Eric Colineau, Mark Sierig, et al. "Thermal Properties and Behaviour of Am-Bearing Fuel in European Space Radioisotope Power Systems." Thermo 1, no. 3 (October 15, 2021): 297–331. http://dx.doi.org/10.3390/thermo1030020.

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The European Space Agency is funding the research and development of 241Am-bearing oxide-fuelled radioisotope power systems (RPSs) including radioisotope thermoelectric generators (RTGs) and European Large Heat Sources (ELHSs). The RPSs’ requirements include that the fuel’s maximum temperature, Tmax, must remain below its melting temperature. The current prospected fuel is (Am0.80U0.12Np0.06Pu0.02)O1.8. The fuel’s experimental heat capacity, Cp, is determined between 20 K and 1786 K based on direct low temperature heat capacity measurements and high temperature drop calorimetry measurements. The recommended high temperature equation is Cp(T/K) = 55.1189 + 3.46216 × 102 T − 4.58312 × 105 T−2 (valid up to 1786 K). The RTG/ELHS Tmax is estimated as a function of the fuel thermal conductivity, k, and the clad’s inner surface temperature, Ti cl, using a new analytical thermal model. Estimated bounds, based on conduction-only and radiation-only conditions between the fuel and clad, are established. Estimates for k (80–100% T.D.) are made using Cp, and estimates of thermal diffusivity and thermal expansion estimates of americium/uranium oxides. The lowest melting temperature of americium/uranium oxides is assumed. The lowest k estimates are assumed (80% T.D.). The highest estimated Tmax for a ‘standard operating’ RTG is 1120 K. A hypothetical scenario is investigated: an ELHS Ti cl = 1973K-the RPSs’ requirements’ maximum permitted temperature. Fuel melting will not occur.
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6

Xia, Y., J. Li, R. Zhai, J. Wang, B. Lin, and Q. Zhou. "Application Prospect of Fission-Powered Spacecraft in Solar System Exploration Missions." Space: Science & Technology 2021 (February 26, 2021): 1–15. http://dx.doi.org/10.34133/2021/5245136.

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Fission power is a promising technology, and it has been proposed for several future space uses. It is being considered for high-power missions whose goal is to explore the solar system and even beyond. Space fission power has made great progress when NASA’s 1 kWe Kilowatt Reactor Using Stirling TechnologY (KRUSTY) prototype completed a full power scale nuclear test in 2018. Its success stimulated a new round of research competition among the major space countries. This article reviews the development of the Kilopower reactor and the KRUSTY system design. It summarizes the current missions that fission reactors are being considered as a power and/or propulsion source. These projects include visiting Jupiter and Saturn systems, Chiron, and Kuiper belt object; Neptune exploration missions; and lunar and Mars surface base missions. These studies suggest that the Fission Electric Propulsion (FEP)/Fission Power System (FPS) is better than the Radioisotope Electric Propulsion (REP)/Radioisotope Power System (RPS) in the aspect of cost for missions with a power level that reaches ~1 kWe, and when the power levels reaches ~8 kWe, it has the advantage of lower mass. For a mission that travels further than ~Saturn, REP with plutonium may not be cost acceptable, leaving FEP the only choice. Surface missions prefer the use of FPS because it satisfies the power level of 10’s kWe, and FPS vastly widens the choice of possible landing location. According to the current situation, we are expecting a flagship-level fission-powered space exploration mission in the next 1-2 decades.
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7

Saqr, Khalid, and Mohd Musa. "Critical review of thermoelectrics in modern power generation applications." Thermal Science 13, no. 3 (2009): 165–74. http://dx.doi.org/10.2298/tsci0903165s.

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The thermoelectric complementary effects have been discovered in the nineteenth century. However, their role in engineering applications has been very limited until the first half of the twentieth century, the beginning of space exploration era. Radioisotope thermoelectric generators have been the actual motive for the research community to develop efficient, reliable and advanced thermoelectrics. The efficiency of thermoelectric materials has been doubled several times during the past three decades. Nevertheless, there are numerous challenges to be resolved in order to develop thermoelectric systems for our modern applications. This paper discusses the recent advances in thermoelectric power systems and sheds the light on the main problematic concerns which confront contemporary research efforts in that field.
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8

Хвостиков, В. П., В. С. Калиновский, С. В. Сорокина, О. А. Хвостикова, and В. М. Андреев. "Тритиевые источники электропитания на основе гетероструктур AlGaAs/GaAs." Письма в журнал технической физики 45, no. 23 (2019): 30. http://dx.doi.org/10.21883/pjtf.2019.23.48716.17941n.

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We report on the development of a radioisotope power source based on the AlхGaAs1-х/GaAs semiconductor converter of β-radiation and tritium as a radiation source. The transducer efficiencies are compared for three types of β-radiation sources: (i) the tritiated titanium disk, (ii) the tritium lamp of green luminescent glow, and (iii) gaseous tritium. When using a converter based on the Al0.35Ga0.65As/GaAs heterostructure in a tritium capsule, the efficiency η = 5.9% is found with the maximum output specific electric power of 0.56 µW/cm2. Due to the prolonged operational life, such autonomous and compact power sources can be utilized in space technology, underwater systems, growth implants, biomedical sensors, and portable mobile equipment of high realibility.
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9

Barco, Alessandra, Richard M. Ambrosi, Hugo R. Williams, and Keith Stephenson. "Radioisotope power systems in space missions: Overview of the safety aspects and recommendations for the European safety case." Journal of Space Safety Engineering 7, no. 2 (June 2020): 137–49. http://dx.doi.org/10.1016/j.jsse.2020.03.001.

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10

Ambrosi, Richard M., Daniel P. Kramer, Emily Jane Watkinson, Ramy Mesalam, and Alessandra Barco. "A Concept Study on Advanced Radioisotope Solid Solutions and Mixed-Oxide Fuel Forms for Future Space Nuclear Power Systems." Nuclear Technology 207, no. 6 (April 21, 2021): 773–81. http://dx.doi.org/10.1080/00295450.2021.1888616.

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11

Parveen, S., S. Victor Vedanayakam, and R. Padma Suvarna. "Thermoelectric generator electrical performance based on temperature of thermoelectric materials." International Journal of Engineering & Technology 7, no. 3.29 (August 24, 2018): 189. http://dx.doi.org/10.14419/ijet.v7i3.29.18792.

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In space applications, the radioisotope thermoelectric generators are being used for the power generation. The energy storage devices like fuel cells, solar cells cannot function in remote areas, in such cases the power generating systems can work successfully for generating electrical power in space missions. The efficiency of thermo electric generators is around 5% to 8% . Bismuth telluride has high electrical conductivity (1.1 x 105S.m /m2) and very low thermal conductivity (1.20 W/ m.K). A Thermoelectric generator has been built up consisting of a Bi2Te3 based on thermoelectric module. The main aim of this is when four thermoelectric modules are connected in series, the power and efficiency was calculated. The thermoelectric module used is TEP1-1264-1.5. This thermoelectric module is having a size of 40mmx40mm. The hot side maximum temperature was 1600C where the cold side temperature is at 400C. At load resistance, 15Ω the maximum efficiency calculated was 6.80%, at temperature of 1600C. The maximum power at this temperature was 15.01W, the output voltage is 16.5V, and the output current is 0.91A. The related and the corresponding graphs between efficiency, power, output voltage, output current was drawn at different temperatures. The efficiency of bismuth telluride, thermoelectric module is greater than other thermoelectric materials.
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12

Tritt, Terry M., and M. A. Subramanian. "Thermoelectric Materials, Phenomena, and Applications: A Bird's Eye View." MRS Bulletin 31, no. 3 (March 2006): 188–98. http://dx.doi.org/10.1557/mrs2006.44.

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AbstractHigh-efficiency thermoelectric (TE) materials are important for power-generation devices that are designed to convert waste heat into electrical energy.They can also be used in solid-state refrigeration devices.The conversion of waste heat into electrical energy may play an important role in our current challenge to develop alternative energy technologies to reduce our dependence on fossil fuels and reduce greenhouse gas emissions.An overview of various TE phenomena and materials is provided in this issue ofMRS Bulletin. Several of the current applications and key parameters are defined and discussed.Novel applications of TE materials include biothermal batteries to power heart pacemakers, enhanced performance of optoelectronics coupled with solid-state TE cooling, and power generation for deep-space probes via radioisotope TE generators.A number of different systems of potential TE materials are currently under investigation by various research groups around the world, and many of these materials are reviewed in the articles in this issue.These range from thin-film superlattice materials to large single-crystal or polycrystalline bulk materials, and from semiconductors and semimetals to ceramic oxides.The phonon-glass/electron-crystal approach to new TE materials is presented, along with the role of solid-state crystal chemistry.Research criteria for developing new materials are highlighted.
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13

Cook, Bruce. "Silicon–Germanium: The Legacy Lives On." Energies 15, no. 8 (April 18, 2022): 2957. http://dx.doi.org/10.3390/en15082957.

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Alloy systems comprised of silicon with germanium, lead with tellurium, and bismuth with antimony have constituted a majority of thermoelectric applications during the last half-century. These legacy materials are primarily covalently bonded with a maximum ZT near one. Silicon–germanium alloys have provided the thermal to electrical conversion for many of NASA’s radioisotope thermoelectric generator (RTG) configurations and for nearly all of its deep space and outer planetary flights, such as Pioneer I and II, Voyager I and 11, Ulysses, Galileo, and Cassini. The remarkable success of these materials and their respective devices is evidenced by the fact that there has never been a failure of the RTG systems even after over 1 billion cumulative mission-hours. The history of this alloy system as a thermoelectric conversion material spans over six decades and research to further improve its performance continues to this day. Si-Ge alloys have long been a mainstay of thermoelectric research because of a fortuitous combination of a sufficiently high melting temperature, reasonable energy band gap, high solubility for both n- and p-type dopants, and the fact that this alloy system exhibits complete miscibility in the solid state, which enable tuning of both electrical and thermal properties. This article reviews the history of silicon–germanium as a thermoelectric material and its use in NASA’s RTG programs. Since the device technology is also a critical operational consideration, a brief review of some of the unique challenges imposed by the use in an RTG is also discussed.
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14

Solórzano, Carlos Renato Huaura, Antonio Fernando Bertachini de Almeida Prado, and Alexander Alexandrovich Sukhanov. "Analysis of Electric Propulsion System for Exploration of Saturn." Mathematical Problems in Engineering 2009 (2009): 1–14. http://dx.doi.org/10.1155/2009/756037.

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Exploration of the outer planets has experienced new interest with the launch of the Cassini and the New Horizons Missions. At the present time, new technologies are under study for the better use of electric propulsion system in deep space missions. In the present paper, the method of the transporting trajectory is used to study this problem. This approximated method for the flight optimization with power-limited low thrust is based on the linearization of the motion of a spacecraft near a keplerian orbit that is close to the transfer trajectory. With the goal of maximizing the mass to be delivered in Saturn, several transfers were studied using nuclear, radioisotopic and solar electric propulsion systems.
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15

Matthes, Christopher S. R., David F. Woerner, and Terry J. Hendricks. "Risk management for dynamic Radioisotope Power Systems." Journal of Space Safety Engineering 5, no. 1 (March 2018): 3–8. http://dx.doi.org/10.1016/j.jsse.2017.11.002.

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16

Lange, Robert G., and Wade P. Carroll. "Review of recent advances of radioisotope power systems." Energy Conversion and Management 49, no. 3 (March 2008): 393–401. http://dx.doi.org/10.1016/j.enconman.2007.10.028.

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17

El-Genk, Mohamed S., and Hamed H. Saber. "Thermal and performance analyses of efficient radioisotope power systems." Energy Conversion and Management 47, no. 15-16 (September 2006): 2290–307. http://dx.doi.org/10.1016/j.enconman.2005.11.022.

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18

Lutz, Steven A., and Chris C. Chan. "Ablation response testing of simulated radioisotope power supplies." Journal of Spacecraft and Rockets 31, no. 3 (May 1994): 489–92. http://dx.doi.org/10.2514/3.26465.

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19

Barco, Alessandra, Richard M. Ambrosi, Christophe Fongarland, Pierre Brunet, Yann Guguin, and Keith Stephenson. "Impact tests and modelling for the ESA radioisotope power systems." Journal of Space Safety Engineering 9, no. 1 (March 2022): 56–71. http://dx.doi.org/10.1016/j.jsse.2021.11.001.

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20

Schriener, Timothy M., and Mohamed S. El-Genk. "Thermal analyses of high-power advanced thermoacoustic radioisotope power system for future space exploration missions." Nuclear Engineering and Design 385 (December 2021): 111504. http://dx.doi.org/10.1016/j.nucengdes.2021.111504.

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21

O'Brien, R. C., and J. A. Katalenich. "Mixed Americium-Curium Heat Sources for Radioisotope Heaters and Power Systems." Journal of Propulsion and Power 27, no. 5 (September 2011): 1131–34. http://dx.doi.org/10.2514/1.b34089.

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22

Watkinson, E. J., R. M. Ambrosi, D. P. Kramer, H. R. Williams, M. J. Reece, K. Chen, M. J. Sarsfield, et al. "Sintering trials of analogues of americium oxides for radioisotope power systems." Journal of Nuclear Materials 491 (August 2017): 18–30. http://dx.doi.org/10.1016/j.jnucmat.2017.04.028.

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23

El-Genk, Mohamed S., and Hamed H. Saber. "Performance analysis of cascaded thermoelectric converters for advanced radioisotope power systems." Energy Conversion and Management 46, no. 7-8 (May 2005): 1083–105. http://dx.doi.org/10.1016/j.enconman.2004.06.019.

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24

Underwood, M. L., D. O'Connor, R. M. Williams, B. Jeffries-Nakamura, M. A. Ryan, and C. P. Bankston. "Electrode performance parameters for a radioisotope-powered AMTEC for space power applications." Journal of Propulsion and Power 8, no. 4 (July 1992): 878–82. http://dx.doi.org/10.2514/3.23564.

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25

Brekis, Arturs, Antoine Alemany, Olivier Alemany, and Augusto Montisci. "Space Thermoacoustic Radioisotopic Power System, SpaceTRIPS: The Magnetohydrodynamic Generator." Sustainability 13, no. 23 (December 6, 2021): 13498. http://dx.doi.org/10.3390/su132313498.

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Electricity production is a major problem for deep space exploration. The possibility of using radioisotope elements with a very long life as an energy source was investigated in the framework of an EU project “SpaceTRIPS”. For this, a two-stage system was tested, the first in which thermal energy is converted into mechanical energy by means of a thermoacoustic process, and the second where mechanical energy is converted into electrical energy by means of a magnetohydrodynamic generator (MHD). The aim of the present study is to develop an analytical model of the MHD generator. A one-dimensional model is developed and presented that allows us to evaluate the behavior of the device as regards both electromagnetic and fluid-dynamic aspects, and consequently to determine the characteristic values of efficiency and power.
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26

TAKIZUKA, Takakazu, Hideshi YASUDA, and Makoto HISHIDA. "Recent space nuclear power systems." Journal of the Atomic Energy Society of Japan / Atomic Energy Society of Japan 33, no. 2 (1991): 116–23. http://dx.doi.org/10.3327/jaesj.33.116.

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27

Kusic, G. L., W. H. Allen, E. W. Gholdston, and R. F. Beach. "Security for space power systems." IEEE Transactions on Power Systems 5, no. 1 (1990): 140–47. http://dx.doi.org/10.1109/59.49098.

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28

Kusic, G. L., W. H. Allen, E. W. Gholdston, and R. F. Beach. "Security for space power systems." IEEE Transactions on Power Systems 5, no. 4 (1990): 1068–75. http://dx.doi.org/10.1109/59.99354.

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29

Hamilton, Ian, and Nisarg Patel. "Nuclear Batteries for Maritime Applications." Marine Technology Society Journal 53, no. 4 (July 1, 2019): 26–28. http://dx.doi.org/10.4031/mtsj.53.4.5.

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AbstractThe large size of the ocean stretches the capability of conventional power sources beyond their limits. Chemical batteries simply do not have enough energy density to power underwater unmanned vehicles (UUVs) for hundreds of miles or oceanic sensors for months on end. Wave and solar energy harvesters are traditionally limited to the surface and cannot provide power to deep water devices. A new type of power supply must be developed if the deep oceans are to be completely mapped and explored. One source of energy that has the power density needed is that of the radioisotope power supply or nuclear battery. This concept draws on the benefits of nuclear power in batteries—just like nuclear submarines use nuclear reactors. Nuclear batteries have energy densities thousands of times greater than chemical cells and can provide power nonstop for months to centuries, depending on the isotope used. Radioisotope batteries do not suffer from the temperature and pressure limitations that conventional batteries do. However, current nuclear battery designs are far too expensive for commercial use and are limited to high-profile applications like space power. A new type of nuclear power supply needs to be developed in order to completely take advantage of radioisotope battery benefits. The authors are developing such a system that makes use of the thermionic energy conversion to create an efficient, cost-effective, and safe nuclear battery, specifically for oceanic applications.
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30

Gatti, Giuliano, and Dudley Perring. "Microwave power amplifiers for space systems." Annales Des Télécommunications 48, no. 7-8 (July 1993): 420–26. http://dx.doi.org/10.1007/bf02995468.

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31

Ehsani, M., M. O. Bilgic, A. D. Patton, and J. Mitra. "New architectures for space power systems." IEEE Aerospace and Electronic Systems Magazine 10, no. 8 (1995): 3–8. http://dx.doi.org/10.1109/62.406815.

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32

Gayathri, S., and K. M. Govindaraju. "Validating a Sign to Forecast the Chemistry of the Fuelused in Radioisotope Power Systems." Indian Journal of Public Health Research & Development 8, no. 3s (2017): 216. http://dx.doi.org/10.5958/0976-5506.2017.00289.3.

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33

Sarsfield, M. J., C. Campbell, C. Carrigan, M. J. Carrott, J.-Y. Colle, D. Freis, C. Gregson, et al. "The Separation of 241Am from Aged Plutonium Dioxide for use in Radioisotope Power Systems." E3S Web of Conferences 16 (2017): 05003. http://dx.doi.org/10.1051/e3sconf/20171605003.

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34

El-Genk, Mohamed S., and Jean-Michel Tournier. "Design optimization and integration of nickel/Haynes-25 AMTEC cells into radioisotope power systems." Energy Conversion and Management 41, no. 16 (November 2000): 1703–28. http://dx.doi.org/10.1016/s0196-8904(00)00021-2.

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35

Kitamura, Shoji, Hiroshi Aoki, Yasushi Okawa, and Hirofumi Taniguchi. "Study of space transportation for space solar power systems." Acta Astronautica 60, no. 1 (January 2007): 1–6. http://dx.doi.org/10.1016/j.actaastro.2006.05.002.

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36

Rinehart, Gary H. "Design characteristics and fabrication of radioisotope heat sources for space missions." Progress in Nuclear Energy 39, no. 3-4 (January 2001): 305–19. http://dx.doi.org/10.1016/s0149-1970(01)00005-1.

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Tagliafico, L. A., and M. Fossa. "Liquid sheet radiators for space power systems." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 213, no. 6 (June 1999): 399–406. http://dx.doi.org/10.1243/0954410991533115.

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Weeks, D. J., and S. A. Starks. "Advanced automation approaches for space power systems." IEEE Computer Applications in Power 2, no. 4 (October 1989): 13–16. http://dx.doi.org/10.1109/67.39143.

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Flood, Dennis J. "Photovoltaics for high capacity space power systems." Acta Astronautica 19, no. 10 (October 1989): 805–12. http://dx.doi.org/10.1016/0094-5765(89)90017-9.

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40

Skorlygin, V. V. "Space Nuclear Power Systems Startup Optimization Methods." Atomic Energy 128, no. 2 (June 2020): 65–70. http://dx.doi.org/10.1007/s10512-020-00652-0.

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41

Novikov, S. G., A. S. Kadochkin, A. V. Berintsev, V. V. Svetukhin, and A. S. Alekseyev. "Simulating of Radioluminescent Compositions based on Microparticles of 63Ni for Radioisotope Power Sources." Nano- i Mikrosistemnaya Tehnika 21, no. 3 (March 27, 2019): 143–53. http://dx.doi.org/10.17587/nmst.21.143-153.

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42

Onufriev, V. V., S. D. Grishin, M. K. Marakhtanov, and V. V. Sinyavskii. "Choice of parameters for current conversion systems in high-power space nuclear power systems." Atomic Energy 89, no. 1 (July 2000): 587–90. http://dx.doi.org/10.1007/bf02673520.

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43

Zhao, Chen, Jiwei Ren, Lin lei, Feiyi Liao, Kezhao Liu, and Yiying Zhao. "X-ray radioluminescent battery with near milliwatt output power using CsI:Tl single crystal scintillator." Applied Physics Letters 121, no. 12 (September 19, 2022): 123906. http://dx.doi.org/10.1063/5.0109011.

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Low output power has long been the bottleneck of micro-radioisotope batteries as power supplies for the wireless sensor network, implantable medical equipment, and outer space exploration. Recently, x-ray radioluminescent batteries demonstrated the great potential to break the deadlock. In this work, we fabricated an x-ray radioluminescent battery with near milliwatt output power and demonstrated various potential applications. A 100% improvement on the conversion efficiency of 2.46% and the highest output power of 136.1 μW/cm2 were achieved when adopting a thallium doped cesium iodide (CsI:Tl) single-crystal scintillator in the battery. Subsequently, a 2 × 2 battery array was fabricated with a maximum output power of 466.9 μW and was used to power devices including micro-LEDs and a wireless sensor system with temperature monitoring. This demo system shows the feasibility of x-ray radioluminescent batteries as a long-lifetime micropower. The tremendous progress will draw broad attention on micro-nuclear batteries and inspire further exploration on the applications in the field of medical devices, space explorations, and Internet of Things.
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Usherovich, Samuel, Crystal Penner, Geoff Hodgson, Edward Thoeng, Morgan Dehnel, and Cornelia Hoehr. "Optical fibre array detector to monitor irradiations for medical radioisotope production." Journal of Physics: Conference Series 2374, no. 1 (November 1, 2022): 012182. http://dx.doi.org/10.1088/1742-6596/2374/1/012182.

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Low-energy cyclotrons are in use worldwide to produce medical radioisotopes for nuclear medicine. Beam monitoring during the irradiation of targets is difficult due to the high-power density of low-energy protons, space limitations, and interference with beam delivery. Doped silica fibres are sensitive to prompt ionizing radiation from the bombarded target, and produce radiation induced luminescence (RIL) when exposed. The fibres can be attached to the outside of the target in a low-profile fibre array, ensuring efficient and safe operation. Here, we present the results from our prototype of such a fibre array. It consists of four Ce-doped fibres with a diameter of 200 μm and has been installed at the TR13 medical cyclotron at TRIUMF where it has been tested at different irradiation conditions.
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Cecati, Federico, Rongwu Zhu, Marco Liserre, and Xiongfei Wang. "Nonlinear Modular State-Space Modeling of Power-Electronics-Based Power Systems." IEEE Transactions on Power Electronics 37, no. 5 (May 2022): 6102–15. http://dx.doi.org/10.1109/tpel.2021.3127746.

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46

SASAKI, Susumu, Tatsuhito FUJITA, and Daisuke JOUDOI. "F191001 Outline of Space Solar Power Systems(SSPS)." Proceedings of Mechanical Engineering Congress, Japan 2011 (2011): _F191001–1—_F191001–3. http://dx.doi.org/10.1299/jsmemecj.2011._f191001-1.

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Sudhoff, S. D., S. F. Glover, P. T. Lamm, D. H. Schmucker, and D. E. Delisle. "Admittance space stability analysis of power electronic systems." IEEE Transactions on Aerospace and Electronic Systems 36, no. 3 (2000): 965–73. http://dx.doi.org/10.1109/7.869516.

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Sudhoff, S. D., S. F. Glover, P. T. Lamm, D. H. Schmucker, D. E. Delisle, and S. P. Karatsinides. "Admittance space stability analysis of power electronic systems." IEEE Transactions on Aerospace and Electronic Systems 36, no. 3 (July 2000): 965–73. http://dx.doi.org/10.1109/7.869517.

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Akimov, V. N., A. A. Koroteev, and A. S. Koroteev. "Space nuclear power systems: Yesterday, today, and tomorrow." Thermal Engineering 59, no. 13 (December 2012): 953–59. http://dx.doi.org/10.1134/s0040601512130022.

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50

Pirjola, R., A. Viljanen, A. Pulkkinen, and O. Amm. "Space weather risk in power systems and pipelines." Physics and Chemistry of the Earth, Part C: Solar, Terrestrial & Planetary Science 25, no. 4 (January 2000): 333–37. http://dx.doi.org/10.1016/s1464-1917(00)00027-1.

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