Relevant bibliographies by topics / Space Radioisotope Power Systems

Academic literature on the topic 'Space Radioisotope Power Systems'

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Published: 10 December 2022
Last updated: 28 January 2023

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Journal articles on the topic "Space Radioisotope Power Systems"

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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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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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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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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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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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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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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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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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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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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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Dissertations / Theses on the topic "Space Radioisotope Power Systems"

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Langham, Ryan C. "Feasibility study and system architecture of radioisotope thermoelectric generation power systems for usmc forward operating bases." Monterey California. Naval Postgraduate School, 2013. http://hdl.handle.net/10945/34695.

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This study sought to identify the feasibility of utilizing a radioisotope thermal (thermoelectric/stirling) generator to provide power to a deployed USMC Expeditionary Force. The conceptual system architecture was constructed through use of the systems engineering process, identifying necessary subsystems and integration boundaries. Radioisotope comparison was then performed, utilizing weighted design factors. It was determined that Sr-90, Cs-137, and Cm-244 would be the most effective fuel sources for this mission area. By analyzing current thermoelectric technology, it was determined that maximum system efficiency is limited to 1015 percent when utilizing available lead telluride thermoelectrics. Barriers to development of identified physical subsystem components were then identified, including health and environmental hazards of potential isotopes, as well as shielding criteria. The system development was found to be feasible and additional design work and development work is proposed.
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Watkinson, Emily Jane. "Space nuclear power systems : enabling innovative space science and exploration missions." Thesis, University of Leicester, 2017. http://hdl.handle.net/2381/40461.

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The European Space Agency’s (ESA’s) 241Am radioisotope power systems (RPSs) research and development programme is ongoing. The chemical form of the americium oxide ‘fuel’ has yet to be decided. The fuel powder will need to be sintered. The size and shape of the oxide powder particles are expected to influence sintering. The current chemical flow-sheet creates lath-shaped AmO2. Investigations with surrogates help to minimise the work with radioactive americium. This study has proposed that certain cubic Ce1-xNdxO2-(x/2) oxides (Ia-3 crystal structures with 0.5 < x < 0.7) could be potential surrogates for some cubic AmO2-(x/2) phases. A new wet-chemical-synthesis-based process for fabricating Ce1-xNdxO2-(x/2) with a targeted x-values has been demonstrated. It uses a continuous oxalate coprecipitation and calcination route. An x of 0.6 was nominally targeted. Powder X-ray diffraction (PXRD) and Raman spectroscopy confirmed its Ia-3 structure. An increase in precipitation temperature (25 °C to 60 °C) caused an increase in oxalate particle median size. Lath/plate-shaped particles were precipitated. Ce Nd oxide PXRD data was Rietveld refined to precisely determine its lattice parameter. The data will be essential for future sintering trials with the oxide where variations in its crystal structure during sintering will be investigated. Sintering investigations with micrometric CeO2 and Nd2O3 have been conducted to understand how AmO2 and Am2O3 may sinter. This is the first reported pure Nd2O3 spark plasma sintering (SPS) investigation. A comparative study on the SPS and the cold-press-and-sinter of CeO2 has been conducted. This is the first study to report sintering lath-shaped CeO2 particles. Differences in their sizes and specific surface areas affected powder cold-pressing and caused variations in cold-pressed-and-sintered CeO2 relative density and Vickers hardness. The targeted density range (85-90%) was met using both sintering techniques. The cold-press-and-sinter method created intact CeO2 discs with reproducible geometry and superior Vickers hardness to those made by SPS.
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Perez-Davis, Marla Esther. "Heat receivers for solar dynamic space power systems." Case Western Reserve University School of Graduate Studies / OhioLINK, 1991. http://rave.ohiolink.edu/etdc/view?acc_num=case1055525095.

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Taylor, Gareth Andrew. "A high voltage transmission line for space power systems." Thesis, University of Newcastle Upon Tyne, 1990. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.315620.

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Presby, Andrew L. "Thermophotovoltaic energy conversion in space nuclear reactor power systems." Thesis, Monterey, Calif. : Naval Postgraduate School, 2004. http://edocs.nps.edu/npspubs/scholarly/theses/2004/Dec/04Dec%5FPresby.pdf.

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Thesis (Astronautical Engineer and M. S. in Astronautical Engineering)--Naval Postgraduate School, December 2004.
Thesis Advisor(s): Gopinath, Ashok ; Michael, Sherif. "December 2004." Description based on title screen as viewed on March 13, 2009. Includes bibliographical references (p. 123-127). Also available in print.
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McGinnis, Scott James. "Nuclear power systems for human mission to Mars /." Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2004. http://library.nps.navy.mil/uhtbin/hyperion/04Dec%5FMcGinnis.pdf.

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Arana, Andrew Jex. "Power Systems Analysis in the Power-Angle Domain." Diss., Virginia Tech, 2009. http://hdl.handle.net/10919/30001.

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The idea of performing power systems dynamic analysis in the power-angle domain has been hinted at by previous researchers, but this may be the first published document to develop detailed techniques by which entire power systems can be represented and solved in the power-angle domain. With the widespread deployment of phasor measurement units and frequency data recorders the industry is looking for more real-time analytical tools to turn real-time wide-area measurements into useful information. Applications based on power-angle domain analysis are simple enough that they may be used online. Power-angle domain analysis is similar to DC load-flow techniques in that a flat voltage profile is used and it is assumed that real power and voltage angle are completely decoupled from reactive power and voltage magnitude. The linearized equations for the dynamics of generators and loads are included in the model, which allows the electromechanical response to be solved using conventional circuit analysis techniques. The effect of generation trips, load switching, and line switching can be quickly approximated with nodal analysis or mesh analysis in the power-angle domain. The analysis techniques developed here are not intended to be as accurate as time-domain simulation, but they are simpler and fast enough to be put online, and they also provide a better analytical insight into the system. Power-angle domain analysis enables applications that are not readily available with conventional techniques, such as the estimation of electromechanical propagation delays based on system parameters, the formulation of electromechanical equivalents, modal analysis, stability analysis, and event location and identification based on a small number of angle or frequency measurements. Fault studies and contingency analysis are typically performed with detailed time-domain simulations, where the electromechanical response of the system is a function of every machine in the interconnection and the lines connecting them. All of this information is rarely known for the entire system for each operating condition; as a result, for many applications it may be more suitable to compute an approximation of the system response based on the current operating state of only the major lines and generators. Power-angle domain analysis is adept at performing such approximations.
Ph. D.
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Yuan, Lin. "Design space re-engineering for power minimization in modern embedded systems." College Park, Md. : University of Maryland, 2006. http://hdl.handle.net/1903/3651.

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Thesis (Ph. D.) -- University of Maryland, College Park, 2006.
Thesis research directed by: Electrical Engineering. Title from t.p. of PDF. Includes bibliographical references. Published by UMI Dissertation Services, Ann Arbor, Mich. Also available in paper.
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McGinnis, Scott J. "Nuclear power systems for human mission to Mars." Thesis, Monterey California. Naval Postgraduate School, 2004. http://hdl.handle.net/10945/1214.

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Nuclear power is the next enabling technology in manned exploration of the solar system. Scientists and engineers continue to design multi-megawatt power systems, yet no power system in the 100 kilowatt, electric, range has been built and flown. Technology demonstrations and studies leave a myriad of systems from which decision makers can choose to build the first manned space nuclear power system. While many subsystem engineers plan in parallel, an accurate specific mass value becomes an important design specification, which is still uncertain. This thesis goes through the design features of the manned Mars mission, its power system requirements, their design attributes as well as their design faults. Specific mass is calculated statistically as well as empirically for 1-15MWe systems. Conclusions are presented on each subsystem as well as recommendations for decision makers on where development needs to begin today in order for the mission to launch in the future.
Lieutenant, United States Navy
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Campbell, Angela Mari. "Architecting aircraft power distribution systems via redundancy allocation." Diss., Georgia Institute of Technology, 2014. http://hdl.handle.net/1853/53087.

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Recently, the environmental impact of aircraft and rising fuel prices have become an increasing concern in the aviation industry. To address these problems, organizations such as NASA have set demanding goals for reducing aircraft emissions, fuel burn, and noise. In an effort to reach the goals, a movement toward more-electric aircraft and electric propulsion has emerged. With this movement, the number of critical electrical loads on an aircraft is increasing causing power system reliability to be a point of concern. Currently, power system reliability is maintained through the use of back-up power supplies such as batteries and ram-air-turbines (RATs). However, the increasing power requirements for critical loads will quickly outgrow the capacity of the emergency devices. Therefore, reliability needs to be addressed when designing the primary power distribution system. Power system reliability is a function of component reliability and redundancy. Component reliability is often not determined until detailed component design has occurred; however, the amount of redundancy in the system is often set during the system architecting phase. In order to meet the capacity and reliability requirements of future power distribution systems, a method for redundancy allocation during the system architecting phase is needed. This thesis presents an aircraft power system design methodology that is based upon the engineering decision process. The methodology provides a redundancy allocation strategy and quantitative trade-off environment to compare architecture and technology combinations based upon system capacity, weight, and reliability criteria. The methodology is demonstrated by architecting the power distribution system of an aircraft using turboelectric propulsion. The first step in the process is determining the design criteria which includes a 40 MW capacity requirement, a 20 MW capacity requirement for the an engine-out scenario, and a maximum catastrophic failure rate of one failure per billion flight hours. The next step is determining gaps between the performance of current power distribution systems and the requirements of the turboelectric system. A baseline architecture is analyzed by sizing the system using the turboelectric system power requirements and by calculating reliability using a stochastic flow network. To overcome the deficiencies discovered, new technologies and architectures are considered. Global optimization methods are used to find technology and architecture combinations that meet the system objectives and requirements. Lastly, a dynamic modeling environment is constructed to study the performance and stability of the candidate architectures. The combination of the optimization process and dynamic modeling facilitates the selection of a power system architecture that meets the system requirements and objectives.
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Books on the topic "Space Radioisotope Power Systems"

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Space nuclear radioisotope systems. Lakewood, Colo: Polaris Books, 2011.

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Radioisotope power systems: An imperative for maintaining U.S. leadership in space exploration. Washington, D.C: National Academies Press, 2009.

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Shipbaugh, Calvin. Power systems for space exploration. Santa Monica, Calif: Rand, 1992.

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Shipbaugh, Calvin. Power systems for space exploration. Santa Monica, Calif: Rand, 1992.

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Nuclear space power and propulsion systems. Reston, Va: American Institute of Aeronautics and Astronautics, 2008.

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Nev.) SAE Power Systems Conference (2004 Reno. Power systems proceedings, 2004. Warrendale, PA: Society of Automotive Engineers, Inc, 2004.

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H, Smith J. Spaceborne power systems preference analyses. [Washington, D.C: National Aeronautics and Space Administration, 1985.

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SAE Aerospace Power Systems Conference (1999 Mesa, Ariz.). Aerospace Power Systems Conference proceedings. Warrendale, Pa: Society of Automotive Engineers, 1999.

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SAE Aerospace Power Systems Conference (1998 Williamsburg, Va.). Aerospace Power Systems Conference proceedings. Warrendale, Pa: Society of Automotive Engineers, 1998.

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SAE Aerospace Power Systems Conference (1999 Mesa, Ariz.). Aerospace Power Systems Conference proceedings. Warrendale, Pa: Society of Automotive Engineers, 1999.

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Book chapters on the topic "Space Radioisotope Power Systems"

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Sheppard, Gareth, Karl Tassenberg, Ramy Mesalam, Bogdan Nenchev, Joel Strickland, and Hugo Williams. "Manufacture of Porous Frit Vents Using Space Holder Methodology for Radioisotopic Space Power Systems." In Characterization of Minerals, Metals, and Materials 2021, 201–10. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-65493-1_19.

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Veltman, André, Duco W. J. Pulle, and R. W. De Doncker. "Space Vector Based Transformer Models." In Power Systems, 157–73. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-29409-4_6.

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Genta, Giancarlo. "Power Systems." In Introduction to the Mechanics of Space Robots, 483–503. Dordrecht: Springer Netherlands, 2012. http://dx.doi.org/10.1007/978-94-007-1796-1_8.

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Amin, Bahram. "Electromagnetic Space Vectors and General Equivalent Circuits." In Power Systems, 13–31. Berlin, Heidelberg: Springer Berlin Heidelberg, 2001. http://dx.doi.org/10.1007/978-3-662-04373-8_2.

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Simmons, Scott. "Space-Based Power Systems." In Human Spaceflight Operations: Lessons Learned from 60 Years in Space, 67–114. Reston, VA: American Institute of Aeronautics and Astronautics, Inc., 2021. http://dx.doi.org/10.2514/5.9781624104770.0067.0114.

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Pelton, Joseph N. "Space-Based Solar Power Satellite Systems." In Space 2.0, 103–14. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-15281-9_8.

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Kunhardt, E. E. "Space Power Experiments Aboard Rockets." In The Behavior of Systems in the Space Environment, 669–711. Dordrecht: Springer Netherlands, 1993. http://dx.doi.org/10.1007/978-94-011-2048-7_27.

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Kukharkin, N. E., N. N. Ponomarev-Stepnoi, and V. A. Usov. "Nuclear Power Sources for Space Systems." In Handbook of Nuclear Chemistry, 2731–58. Boston, MA: Springer US, 2011. http://dx.doi.org/10.1007/978-1-4419-0720-2_59.

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Boteler, D. H. "Space Weather Effects on Power Systems." In Geophysical Monograph Series, 347–52. Washington, D. C.: American Geophysical Union, 2013. http://dx.doi.org/10.1029/gm125p0347.

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Pignolet, G. "Integrating Wireless Power Transportation and Solar Power Systems Studies and Society." In Space of Service to Humanity, 271–75. Dordrecht: Springer Netherlands, 1997. http://dx.doi.org/10.1007/978-94-011-5692-9_30.

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Conference papers on the topic "Space Radioisotope Power Systems"

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Oleson, Steven R., Lisa Kohout, and Ralph Lorenz. "Saturn Spacecraft Power: Trading Radioisotope, Solar, and Fission Power Systems." In AIAA SPACE 2016. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-5361.

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El-Genk, Mohamed S. "Energy Conversion Options for Advanced Radioisotope Power Systems." In SPACE TECHNOLOGY AND APPLICATIONS INT.FORUM-STAIF 2003: Conf.on Thermophysics in Microgravity; Commercial/Civil Next Generation Space Transportation; Human Space Exploration; Symps.on Space Nuclear Power and Propulsion (20th); Space Colonization (1st). AIP, 2003. http://dx.doi.org/10.1063/1.1541316.

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Crowley, Christopher J. "Thermophotovoltaic Converter Performance for Radioisotope Power Systems." In SPACE TECHNOLOGY AND APPLICATIONS INT.FORUM-STAIF 2005: Conf.Thermophys in Micrograv;Conf Comm/Civil Next Gen.Space Transp; 22nd Symp Space Nucl.Powr Propuls.;Conf.Human/Robotic Techn.Nat'l Vision Space Expl.; 3rd Symp Space Colon.; 2nd Symp.New Frontiers. AIP, 2005. http://dx.doi.org/10.1063/1.1867178.

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Eschenbaum, Ronald C., and Michael J. Wiemers. "Design of radioisotope power systems facility." In Proceedings of the eighth symposium on space nuclear power systems. AIP, 1991. http://dx.doi.org/10.1063/1.39984.

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Sholtis, Joseph A., Ronald J. Lipinski, and Mohamed S. El-Genk. "Coated particle fuel for radioisotope power systems (RPSs) and radioisotope heater units (RHUs)." In Space technology and applications international forum -1999. AIP, 1999. http://dx.doi.org/10.1063/1.57532.

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Crowley, Christopher J. "Thermophotovoltaic Converter Design for Radioisotope Power Systems." In SPACE TECHNOLOGY AND APPLICATIONS INTERNAT.FORUM-STAIF 2004: Conf.on Thermophys.in Microgravity; Commercial/Civil Next Gen.Space Transp.; 21st Symp.Space Nuclear Power & Propulsion; Human Space Explor.; Space Colonization; New Frontiers & Future Concepts. AIP, 2004. http://dx.doi.org/10.1063/1.1649641.

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El-Genk, Mohamed S. "Radioisotope Power Systems with Skutterudite-Based Thermoelectric Converters." In SPACE TECHNOLOGY AND APPLICATIONS INT.FORUM-STAIF 2005: Conf.Thermophys in Micrograv;Conf Comm/Civil Next Gen.Space Transp; 22nd Symp Space Nucl.Powr Propuls.;Conf.Human/Robotic Techn.Nat'l Vision Space Expl.; 3rd Symp Space Colon.; 2nd Symp.New Frontiers. AIP, 2005. http://dx.doi.org/10.1063/1.1867164.

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Schaefer, Edward, Douglas Mehoke, Carl Ercol, and Steven Vernon. "Implementation Challenges Using Radioisotope Power Generation in Space Systems." In AIAA SPACE 2007 Conference & Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-6112.

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Howell, Edwin I., Dennis C. McNeil, and Wayne R. Amos. "Development of a radioisotope heat source for the two-watt radioisotope thermoelectric generator." In Proceedings of the ninth symposium on space nuclear power systems. AIP, 1992. http://dx.doi.org/10.1063/1.41871.

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El-Genk, Mohamed S. "Cascaded Thermoelectric Converters for Advanced Radioisotope Power Systems." In SPACE TECHNOLOGY AND APPLICATIONS INTERNAT.FORUM-STAIF 2004: Conf.on Thermophys.in Microgravity; Commercial/Civil Next Gen.Space Transp.; 21st Symp.Space Nuclear Power & Propulsion; Human Space Explor.; Space Colonization; New Frontiers & Future Concepts. AIP, 2004. http://dx.doi.org/10.1063/1.1649614.

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Reports on the topic "Space Radioisotope Power Systems"

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Wei, G. C., and J. M. Robbins. Development and characterization of carbon-bonded carbon fiber insulation for radioisotope space power systems. Office of Scientific and Technical Information (OSTI), June 1985. http://dx.doi.org/10.2172/5567894.

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2

Barnett, W., P. Dick, B. Beaudry, P. Gorsuch, and E. Skrabek. Thermoelectric Alloys and Devices for Radioisotope Space Power Systems: State of the Art and Current Developments. Office of Scientific and Technical Information (OSTI), January 1989. http://dx.doi.org/10.2172/1033425.

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3

Carpenter, Robert, V. Kumar, C. Ore, and Alfred Schock. Effect of Inert Cover Gas on Performance of Radioisotope Stirling Space Power System. Office of Scientific and Technical Information (OSTI), January 2001. http://dx.doi.org/10.2172/1128538.

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4

Daniel P. Kramer and Chadwick D. Barklay. Materials Technology Support for Radioisotope Power Systems Final Report. Office of Scientific and Technical Information (OSTI), October 2008. http://dx.doi.org/10.2172/939895.

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5

Edenburn, M. W. Models for multimegawatt space power systems. Office of Scientific and Technical Information (OSTI), June 1990. http://dx.doi.org/10.2172/6252925.

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6

Smith, William B., Jacob F. Rutten, David L. Armstrong, Thomas J. Farish, and Patrice A. Stevens. Space and Defense Power Systems Maintenance Plan. Office of Scientific and Technical Information (OSTI), June 2013. http://dx.doi.org/10.2172/1084514.

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7

Kuspa, J. P., E. J. Wahlquist, and D. A. Bitz. Important technology considerations for space nuclear power systems. Office of Scientific and Technical Information (OSTI), March 1988. http://dx.doi.org/10.2172/6893131.

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8

Besmann, T. M. Assessment of ceramic composites for multimegawatt space nuclear power systems. Office of Scientific and Technical Information (OSTI), December 1986. http://dx.doi.org/10.2172/6839642.

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9

Werner, James Elmer, Stephen Guy Johnson, Carla Chelan Dwight, and Kelly Lynn Lively. Cost Comparison in 2015 Dollars for Radioisotope Power Systems -- Cassini and Mars Science Laboratory. Office of Scientific and Technical Information (OSTI), July 2016. http://dx.doi.org/10.2172/1364515.

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10

Johnson, Stephen G. Considerations for Use of Am-241 for Heat Source Material for Radioisotope Power Systems. Office of Scientific and Technical Information (OSTI), January 2017. http://dx.doi.org/10.2172/1504930.

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