Advances of Safety Research on Nuclear Space Power Sources

HU Wenjun1, CHEN Hongyong1, CHEN Junhong1, LI Shangming1, HU Shaoquan1, TANG yuhua2

PDF(462 KB)
PDF(462 KB)
Journal of Deep Space Exploration ›› 2017, Vol. 4 ›› Issue (5) : 453-465. DOI: 10.15982/j.issn.2095-7777.2017.05.006

Advances of Safety Research on Nuclear Space Power Sources

  • HU Wenjun1, CHEN Hongyong1, CHEN Junhong1, LI Shangming1, HU Shaoquan1, TANG yuhua2
Author information +
History +

Abstract

The RHU(Radiosotope Heater Unit), RTG (Radioisotope Thermoelectric Generator) and space nuclear reactors have wide applications in deep space exploration missions. The safety principles are investigated based on their technology characteristics and the applications of nuclear sources in outer space are introduced, such as the RHU/RTG of ALRH (Apollo Lunar Radiosotope Heater), GPHS(General Purpose Heater Source) and LWRHU (Lighted Weighted Radiosotope Heater Unit), MMRTG (Multi-Mission Radioisotope Thermoelectric Generator), and space nuclear reactor of TOPAZ-II.The safety tests and analysis done by the United States and Russia are studied, and the safety validation and assess approach are reviewed, The work focuses on the technology details of the tests and analysis of RHU/RTG for different missions. The work would serve as reference for the application of nuclear source in outer space.

Keywords

Radiosotope Heater Unit / Radioisotope Thermoelectric Generator / Space Nuclear Reactor,deep space exploration / safety test

Cite this article

Download citation ▾
HU Wenjun, CHEN Hongyong, CHEN Junhong, LI Shangming, HU Shaoquan, TANG yuhua. Advances of Safety Research on Nuclear Space Power Sources. Journal of Deep Space Exploration, 2017, 4(5): 453‒465 https://doi.org/10.15982/j.issn.2095-7777.2017.05.006

References

[1] Lee H C,Lim H S,Han T Y. A neutronic feasibility study on a small LEU fueled reactor for space applications[J]. Annals of Nuclear Energy. 2015,77:35-46
[2] Les J,Michael M,Bryan P,et al. Development priorities for in-space propulsion technologies[J]. Acta Astronautica. 2013,82:148-152
[3] Bragg-Sitton,Shannon M,et al. Ongoing space nuclear systems development in the United States[C]//2011 International Nuclear Atlantic Conference-INAC 2011.Belo Horizonte:INAC,2011.
[4] 周继时,朱安文,耿言. 空间核能源应用的安全性设计、分析和评价[J]. 深空探测学报,2015,2(4):302-311
Zhou J S,Zhu A W,Gen Y. The safety design,analysis and evaluation of nuclear power application in space[J]. Journal of Deep Space Exploration,2015,12(4):302-311
[5] Rivert A B. Applicability of trends in nuclear safety analysis to space nuclear power systems[J]. Aip Conforence,1993 ,271 (1):435-437
[6] Steven A. Background on space nuclear power[J]. Science &; Global Security,2007 ,1 (1-2) :93-107
[7] Roger XL. Nuclear safety,legal aspects and policy recommendations for space nuclear power and propulsion systems[J]. Acta Astronutica,2006,59:398-412
[8] Gary L B. Space nuclear power:opening the final frontier[C]// 4th International Energy Conversion Engineering Conference and Exhibit. San Diego,California:AIAA,2006.
[9] Dean K. Nuclear security and nuclear emergencey response in China[J]. Science & Global Security,2012,20:30-63
[10] 尹玉海,龙杰.《关于在外层空间使用核动力源的原则》之再思考[J]. 北京航空航天大学学报(社会科学版),2013,26(5): 27-32
YIN Y H. Long J. Reconsideration of the principles relevant to the use of nuclear power sources in outer space[J]. Journal of Beijing University of Aeronautics and Astonautics(Social Sciences Edition),2013,26(5):27-32
[11] 尹玉海,龙杰. 美国外空核动力源安全机制对中国的启示[J]. 北京理工大学学报(社会科学版),2014,16(2):105-111
YIN Y H. Long J. The U.S. outer space nuclear power sources security mechanism and its implication for China[J]. Journal of Beijing Institute of Technology(Social Sciences Edition),2014,16(2):105-111
[12] Committee on the Peaceful Uses of Outer Space. Principles relevant to the use of nuclear sources in outer space[R]. UN G.A. Resolution A/Res/47/68(Dec. 14,1992);GAOR,47th Session,Supp. No. 20,UN Doc,A/47/20,1992.
[13] Summerer L,Wilcox R E,Bechtel R. The International safety framework for nuclear power source applications in outer space-useful and substantial guidance[J]. Acta Astronautica,2015,111,(1):89-101
[14] Roger X L. Nuclear safety,legal aspects and policy recommendations for space nuclear power and propulsion systems[J]. Acta Astronutica,2006,59:398-412
[15] Lyle L R,Meera M,Bart W B. Nuclear Safety Analysis for the Mars Exploration Rover 2003 Project[C]//. Henry Firstenberg,Space Technology and Applications International Forum–STAIF 2004,Albuquerque,[s.n.],2004.
[16] Daniel J C,John B,Christopher A. J.et al. Nuclear Risk Assessment for the Mars 2020 Mission Environmental Impact Statement[R]. Sandia National Laboratories,SANDIA REPORT,SAND2013-10589,January 2014.
[17] Tate,R E,The Light Weight Radioisotope Heater Unit(LWRHU): A Technical Description of the Reference Design[R],Los Alamos National Laboratory,LA-9078-MS,January 1982.
[18] National Aeronautics and Space Administration,Mars Exploration Rover Delta II Final SAR Data book[R]. May 19,2002.
[19] ASCA,Incorporated,Mars 2020 Launch Accident Probability Data for EIS Risk Assessment,Revision Draft,AR 13-02[R]. Prepared for National Aeronautics and Space Administration,Kennedy Space Center,September 2013.
[20] Sforza P M,Shooman M L,Pelaccio D G.A safety and reliability analysis for space nuclear thermal propulsion systems[J]. Acta Astronautica,1993,30:67-83.
[21] Gary L B,Thomas J M. NASA program planning on nuclear electric propulsion[C]// AIAA Space Program and Technologies Conference,Huntsville:AIAA,1992,AIAA-92-1557.
[22] Cooper R H,Moore J P. Materials in space nuclear power systems[R]. CONF-911107-28-Extd.Abst.1991.
[23] Mohamed S E,Michel J T. A review of refractory metal alloys and mechanically alloyed-oxide dispersion strengthened steels for space nuclear power systems[J]. Journal of Nuclear Materials,2005,340:93-112
[24] Wilcox R. Safety in the design and development tof United States space NPS applications[C]// In Scientific and Technical Subcommittee of the Committee on the Peaceful Uses of Outer Space,Volume 48thsession. Vienna,Austria;[s.n.],2011.
[25] Bechtel R D,Lipinski R J,Smith J A. U.S. approach to risk assessment and its role in implementing an effective safety program for space nuclear power sources applications[C]// Scientific and Technical Subcommittee of the Committee on the Peaceful Uses of Outer Space,volume Forty-eighth session. Vienna,Austria;[s.n.],2011.
[26] Bennett,Gary L. “Soviet Space Nuclear Reactor Incidents: perception Versus Reality”,in Space Nuclear Power Systems 1989[M]. Hoover:Orbit Book Company,1992.
[27] Bennett,Gary L. The safety review and approval process for space nuclear power sources[J]. Nuclear Safety,1991,32(1):1-18
[28] Charles O,Grigsby. Comparison of general purpose heat source testing with the ANSI,N43.6-1997(R 1989)[R].[S.l.]:ANSI,1998.
[29] Kelly D P,Avona V L. Apollo lunar radioisotopic heater summary report,MLM-1637[R].1969.
[30] Kelly D P ,Avona V L. Apollo Lunar radioistotopic heater aerothermodynamic summary report,SC-RR-69-125 [R]. 1969.
[31] Rinehart G H. Design characteristics and fabrication of radioisotope heat sources for space missions[J]. Progress in Nuclear Energy,2001,39(1-2):305-319
[32] Safety status report for the Ulysses mission,Accident analysis(Book 1),OSDS4202[R]. 1990.
[33] Final safety analysis report for the Galileo mission,Volume II (Book 1),Accident model document,87SDS4213[R]. 1988.
[34] Bechtel R D,Lipinski R J,Smith J A,et al. U.S. Approach to risk assessment and its role in implementing an effective safety program for space nuclear power sources applications,A/AC.105/C.1/2011/CRP.5.[R]. USA[s.n.],2011.
[35] Cull T A,George T G,Pavone D. General-purpose heat source development safety verification test program: explosion overpressure test series,LA-10697-MS [R]. 1986.
[36] George T G,Tate R E,Axler K M. General-purpose heat source development safety verification test program:bullet/fragment test series ,LA-1036-MS [R]. 1985.
[37] George T G,General-purpose heat source development safety verification test program:titanium bullet/fragment test series ,LA-10724-MS [R]. 1986.
[38] Environmental assessment of general-purpose heat source safety verification testing,DOE/EA-1025 [R]. 1995.
[39] Cull T A,General-purpose heat source development: extended series test program large fragment tests,LA-11597-MS [R]. 1989.
[40] Reimus M A H,Hinckley J E. General-purpose heat source:research and development program,radioisotope thermoelectric generator/thin fragment impact test,LA-13220 [R]. 1996.
[41] Reimus M A H,Hinckley J E,George T.G. General-purpose heat source:research and development program,radioisotope thermoelectric generator impact tests:RTG-1 and RTG-2,LA-13147 [R]. 1996.
[42] Grigsby C O.Comparision of general purpose heat source testing with the ASNI N43.6-1997(R 1989)sealed source standard ,LA-UR-98-1826 [R]. 1998.
[43] Snow E C. Safety test No.S-6,Launch pad abort sequential test phase II: Solid propellant fire,LA-6034-MS [R]. 1975.
[44] Boris G,Oglobin,Yuriy F ,Proshin,and Anatoliy I S. Off-line life tests of Topaz‐2 system reactor unit assembly units[J]. AIP Conference Proceedings,1995,324:713-718
[45] Grinberg E I,Doschatov V V,Usov. Thermal state of the safety system,reactor,side reflector and shielding of the “Topaz-2” system under conditions of fire caused by a launcher accident at the launch pad[J]. AIP Conference Proceedings,1996,361:981 -990
[46] Susan S V,Edward A,Rodriguez.Russian Topaz II system test program(1970-1989)[J].AIP Conference Proceedings,1994,301:803-821
[47] Glen L S,Boris O,Valeri S,et al.Topaz II Non-nuclear qualification test program[J]. AIP Conference Proceedings,1994,301:1185-1191
[48] Luchau D W,Sinkevich V G,Wernsman B,et al. Final report on testing of TOPAZ II unit Ya‐21u:output power characteristics and system capabilities[J]. AIP Conference Proceedings,1996,361,1389-1395
[49] Paramonov,Dmitry V,El-genk,Mohamed S.Analysis of ya-21u thermionic fuel elements[J]. Nuclear Technology,1996,116:261-269
[50] Wold S K.Thermionic system evaluation test facility construction:a United States and Russian effort,SAND-92-2276C [R]. 1993.
[51] Fairchild J F,Koonmen J P,Frank V. Thermionic system evaluation test facility description[J]. AIP conference Proceeding,1992,246:836-842
[52] Morris D B. The thermionic system evaluation test:descriptions,limitations,and the involvement of the space nuclear power community[J]. AIP Conference Proceedings,1993,271:1251-1255.
[53] Polansky G F,Schmidt G L,Voss S S. Evaluating Russian space nuclear reactor technology for United States applations[R]. 1994.
[54] Paternoster R R. TOPAZ-II U.S. critical experiments program[J]. AIP conference Proceeding,1994,301,97:97-101.
[55] Trujillo D,Darrel B,Chris P. Conceptual design of the Topaz II anticriticality device,LA-UR-93-3287 [R]. 1993.
[56] Susan S V. An overview of the nuclear electric propulsion space test program(NEPSTP)satellite,LA-UR-94-1688 [R],1994.
[57] Scott K W. Thermionic system evaluation test(TSET)facility construction:a United States and Russian effort,SAND-92-2276C [R]. 1992.
[58] Jerry F F,James P K,Frank V T. Thermionic system evaluation test(TSET)facility description[J]. AIP conference Proceeding,1992,246:836-842.
[59] The thermionic system evaluation test:descriptions,limitations,and the involvement of the space nuclear power community[J]. AIP Conference Proceedings,1993,271:1251-1255
[60] Connell L W,Trost L C. Reentry safety for the Topaz II space reactor:issues and analysis,SAND94-0484 [R]. 1994.
[61] U.S. approach to risk assessment and its role in implementing an effective safety program for space nuclear power sources applications[C]// Committee on the Peaceful Uses of Outer Space,Scientific and Technical Subcommittee,Vienna:[s.n.],2011.
PDF(462 KB)

Accesses

Citations

Detail

Sections
Recommended

/