[1] 褚桂柏. 航天技术概论 [M]. 北京：中国宇航出版社，2002：60-65.
[2] 萨顿，比布拉兹. 火箭发动机基础 [M]. 北京：科学出版社，2003：20-70.
[3] Enrich W J. Principle of nuclear rocket propulsion [M]. Oxford：Elsevier，2016：31-53.
[4] 张楠,徐智君,朱晓农,等. 激光推进技术[J]. 红外与激光工程,2011,40(6):1025-1037
Zhang N,Xu Z J,Zhu X N,et al. Laser propulsion technology[J]. Infrared and Laser Engineering,2011,40(6):1025-1037
[5] 洪延姬,李修乾,窦志国. 激光推进研究进展[J]. 航空学报,2009,30(11):2003-2015
Hong Y J,Li X Q,Dou Z G. Advances in study of laser propulsion [J]. Acta Aeronautica et astronautica sinica,2009,30(11):2003-2015
[6] 张纯良,高芳,张振鹏,等. 太阳能热推进技术的研究进展[J]. 推进技术,2004,25(2):187-192
Zhang C L,Gao F,Zhang Z P,et al. Investigation and development on solar thermal propulsion[J]. Journal of Propulsion Technology,2004,25(2):187-192
[7] 杭观荣,洪鑫,康小录. 国外空间推进技术现状和发展趋势[J]. 火箭推进,2013,39(5):7-15
Hang G R,Hong X,Kang X L. Current status and development trend of space propulsion technologies abroad [J]. Journal of Rocket Propulsion,2013,39(5):7-15
[8] 刘红军. 新概念推进技术及其应用前景[J]. 火箭推进,2004,30(4):36-40
Liu H J. New concept propulsion systems and their application prospect [J].Journal of Rocket Propulsion,2004,30(4):36-40
[9] 苏著亭，杨继材，柯国土.空间核动力[M]. 上海：上海交通大学出版社，2016：11-58.
[10] Powell J，Ludewig H，Horn F. The liquid annular reactor system propulsion，1991N22145 [R]. New York，USA：Brookhaven National Laboratory，1991.
[11] Robert G. Ragsdale. Status of open-cycle gas-core reactor project through 1970[R]. Cleveland，Ohio，USA：Lewis research center，1971.
[12] Koehlinger M W,Bennett R G,Motloch C G. Gas core nuclear thermal rocket engine research and development in the former USSR[J]. Rockets,1992(4):94
[13] 斯科洛夫. 反应堆材料学[M].北京：原子能出版社，1989：9-91
[14] 段小龙. 载人火星计划空间推进方案的任务性能[J]. 火箭推进,2002,28(6):42-47.
[15] Hoffman S J，Kaplan D J. Human exploration of Mars：the reference mission of the NASA Mars exploration study team，NASA-SP-6107 [R]. NASA：Johnson Space Center，1997.
[16] Drake B G. Reference mission version 3.0 addendum to the human exploration of Mars：the reference mission of the NASA Mars exploration study team [R]. NASA：Johnson Space Center，1998.
[17] Drake B G. Human exploration of Mars design reference architechture5.0[R]. NASA：Johnson Space Center，2009.
[18] Borowski S K，Mccurdy D R，Packard T W. Nuclear thermal rocket/vehicle characteristics and sensitivity trades for NASA’s Mars design reference architecture（DRA）5.0 study [C]//Nuclear and Emerging Technologies for Space 2009. Atlanta，USA：NASA，2009.
[19] 洪刚,娄振,郑孟伟,等. 载人核热火箭登陆火星方案研究[J]. 载人航天,2015,21(6):611-617
Hong G,Lou Z,Zheng M W,et al. Study on nuclear thermal rocket for manned Mars exploration[J]. Manned Spaceflight,2015,21(6):611-617
[20] Zhang Z X,Zheng B,Zhou H,et al. Overall scheme of manned asteroid exploration mission [J]. Journal of Deep Space Exploration,2015 2(3):229-235.
[21] 王开强,张柏楠,王悦,等. 载人小行星探测的任务特点与实施途径探讨[J]. 航天器工程,2014,23(3):105-111
Wang K Q,Zhang B N,Wang Y,et al. Character and technological approach of human asteroid exploration mission [J]. Spacecraft Engineering,2014,23(3):105-111
[22] 李志海,张柏楠,杨宏,等. 载人小行星探测推进技术初步方案设想[J]. 国际太空,2013(7):32-37.
[23] 高朝辉,童科伟,时剑波,等. 载人火星和小行星探测任务初步分析[J]. 深空探测学报,2015,2(1):10-19
Gao C H,Tong K W,Shi J B,et al. Analysis of the manned mars and asteroid missions [J]. Journal of Deep Space Exploration,2015,2(1):10-19
[24] Wang L,Hou X B. Key technologies and some suggestions for the development of space solar power station[J]. Spacecraft Environment Engineering,2014,31(4):343-350.
[25] 张钧屏. 空间太阳能电站构想及其相关技术的发展[J]. 航天返回与遥感,2011,32(5):10-18
Zhang J P. The concept of solar power satellite(SPS)and its key technologies[J]. Space Recovery & remote sensing,2011,32(5):10-18
[26] 高朝辉,王俊峰,童科伟,等. 重型运载火箭发射空间太阳能电站相关技术问题分析[J]. 导弹与航天运载技术,2016(3):51-54
Gao C H,Wang J F,Tong K W,et al. Technology analysis of the questions on space solar-power station launching by the heavy launch vehicles [J]. Missile and Space Vehicles,2016(3):51-54
[27] Beeson R T，Faler A C，Garner R J. Design of an evolvable nuclear thermal rocket ferry for geosynchronous transfer[C]//Nuclear and Emerging Technologies for Space 2014. Slidell，USA：[s.n.]，2014.
[28] 果琳丽,王平,朱恩涌,等. 国外月球基地发展概况[J]. 科技创新导报,2014(27):16-17.
[29] Borowski S，Clark J，Sefcik R，et al. An accelerated development，reduced cost approach to Lunar/Mars exploration using a modular NTR-based space transportation system [R]. Cleveland，USA：Lewis Research Center，1992.
[30] Borowski S K，McCurdy D R，Packard T W. Modular growth NTR space transportation system for future NASA human Lunar，NEA and Mars exploration missions[C]//AIAA SPACE 2012 Conference and Exposition. Pasadena，USA：[s.n.]，2012.
[31] Borowski S K. Nuclear thermal rocket workshop reference system - ROVER/NERVA，92N11091[R].Cleveland，USA：Lewis Research Center，1992.
[32] Donald P M. Los Alamos nuclear rocket project ROVER [R]. Los Alamos，USA：University of California，1963.
[33] Finseth J L. ROVER nuclear rocket engine program：overview of ROVER engine tests final report[R]. Huntsville，USA：Marshall Space Flight Center，1991.
[34] Gary L N. Nuclear thermal propulsion program overview[R]. Washington D C，USA：NASA，1992.
[35] Thomas G R，Arnold W H. NERVA program NRX-A1 test final report[R]. Pennsylvania，USA：Westinghouse Electric Corporation，1964.
[36] James T W. An overview of tested and analyzed NTP concepts[C]//AIAA/NASA/OAI Conference on Advanced SEI Technologies.Cleveland，USA：[s.n.]，1991.
[37] Robbins W H，Finger H B. Anhistorical perspective of the NERVA nuclear rocket engine technology program[C]//AIAA/NASA/OAI Conference on Advanced SEI Technologies.Cleveland，USA：[s.n.]，1991.
[38] Durham F P，Krik W L，Bohl R J. A review of the Los Alamos effort in the development of nuclear rocket propulsion[C]//AIAA/NASA/OAI Conference on Advanced SEI Technologies.Cleveland，USA：[s.n.]，1991.
[39] David L. Black，Stanley V. G. A technical summary of engine and reactor subsystem design performance during the NERVA program[C]//AIAA/NASA/OAI Conference on Advanced SEI Technologies. Cleveland，USA：[s.n.]，1991.
[40] Simmons C R.，Yario W R，Ivins R O. Final report on the testing of graphite-type nuclear rocket fuel in a pulsed reactor，10.2172/4258954 [R]. Illinois，USA：Argonne national laboratory，1964.
[41] Matthews R，Blair H，Chidester K，et al. Carbide fuels for nuclear thermal propulsion[C]//AIAA/NASA/OAI Conference on Advanced SEI Technologies. Cleveland，USA：[s.n.]，1991.
[42] Cooper R H. Materials for space nuclear thermal propulsion system[C]//AIAA/NASA/OAI Conference on Advanced SEI Technologies. Cleveland，USA：[s.n.]，1991.
[43] Lyon L L. Performance of（U，Zr）C-graphite（composite）and of（U，Zr）C（carbide）fuel elements in the nuclear furnace 1 test reactor，10.2172/4419566 [R]. California，USA：Los Alamos laboratory，1973.
[44] Stanly V. G. Development of nuclear rocket engine technology[C]//AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference. Monterey USA：[s.n.]，1989.
[45] Nuclear technology department，Nuclear energy division. 710 high temperature gas reactor program summary report：Volume 1 summary[R]. Ohio，USA：General Electric，1973.
[46] Brengle R G，Harty R B. The promise and challenges of cermet fueled nuclear thermal propulsion reactors [C]//AIAA/SAE/ASME/ASEE 29th Joint Propulsion Conference and Exhibit. Monterey USA：AIAA，1993.
[47] Marchaterre J F. Nuclear rocket program terminal report[R] Illinois，USA：Argonne National Laboratory，1968.
[48] Allen-Beale G，Lawrence T J. The history of nuclear thermal propulsion at the Phillips laboratory[C].//AIAA/NASA/OAI Conference on Advanced SEI technologies，Cleveland，USA：AOAA，1991.
[49] Haslett R A. Space nuclear thermal propulsion program final report，AD-A--305996/1/XAB[R]. Bethpage，USA：Grumman Aerospace Corporation，1995.
[50] Ludewig H,Powell J R,Todosow M,et al. Design of particle bed reactors for the space nuclear thermal propulsion program [J].Nuclear news,1996,30(1):1-65
[51] Horn F L. Seven element blow down experiment-department safety report[R]. New York，USA：Brookhaven National laboratory，1990.
[52] Polansky G F. Comparison of selected nuclear thermal propulsion comcepts[C]//AIAA/NASA/OAI Conference on Advanced SEI technologies. Cleveland，USA：AIAA，1991.
[53] Kerrebrock J L，Kalamas J. Flow instability in particle bed nuclear reactor[C]//AIAA/SAE/ASME/ASEE 29th Joint Propulsion Conference and Exhibit. Monterey USA：AIAA，1993.
[54] Lawrence T J，Powell J. Flow instability tests for a particle bed reactor nuclear thermal rocket fuel element[C]//AIAA/SAE/ASME/ASEE 31st Joint Propulsion Conference and Exhibit. San Diego USA：AIAA，1995.
[55] Brandhorst H W，Cataldo R L. SEI needs for space nuclear power[C]//AIAA/NASA/OAI Conference on Advanced SEI technologies. Cleveland，USA：AIAA，1991.
[56] Cohen A. Report of the 90-day study on human exploration of the Moon and Mars[R]. Washington D C，USA：NASA，1989.
[57] John S C，Stanly K B，Melvin C M. Nuclear thermal propulsion transportation system for Lunar/Mars exploration[C]//Nuclear power engineering in space-nuclear rocket engines. Semipalatinsk，Kazakhstan：[s.n.]，1992.
[58] Stanley K B. The rationale/benefits of nuclear thermal rocket propulsion for NASA’s Lunar space transportation system[C]//AIAA/SAE/ASME/ASEE 27th Joint Propulsion Conference. Sacramento，USA：AIAA，1991.
[59] Parsley R C. Advanced propulsion engine assessment based on a CERMET reactor[C]//Nuclear propulsion TIM.USA：[s.n.]，1992.
[60] Bulman M J，Culver D W，.Mcllwain M C，et al. US/CIS integrated NTRE[C]//AIAA/SAE/ASME/ASEE 29th Joint Propulsion Conference and Exhibit. Monterey USA：[s.n.]，1993.
[61] Peery S D，Parsley R C，Anghaie S，et al. XNR2000—a near term nuclear thermal rocket concept[C]//10th Symposiumù Space Nuclear Power and Propulsion. Maryland，USA：AIP Publishing，2008，271（3）：1743-1752.
[62] Powell J，Maise G，Paniagua J. Phase 1-final report，lightweight high specific impulse space propulsion system[R].New York，USA：Plus Ultra Technologies，1999.
[63] Gouw R R. Nuclear design analysis of square-lattice honeycomb space nuclear rocket engine[D]. Florida：University of Florida，2000.
[64] 李虹琳. 美国的载人小行星和火星探测[J]. 中国航天,2014(8):45-50.
[65] Houts M G，Borowski S K，George J A，et al. Nuclear cryogenic propulsion stage[C]//Nuclear and Emerging Technologies for Space 2012.The Woodlands，USA：[s.n.]，2012.
[66] Trammell M P，Jolly B C，Miller J H，et al. Recapturing graphite-based fuel element technology for Nnuclear thermal propulsion[C]//AIAA/ASME/SAE/ASEE 49th Joint Propulsion Conference and Exhibit. San Jose，USA：AIAA，2013.
[67] Hickman R R，Broadway J W，Mireles O R. Fabrication and testing of CERMET fuel materials for nuclear thermal propulsion[C]//AIAA/ASME/SAE/ASEE 48th Joint Propulsion Conference and Exhibit. Atlanta，USA：AIAA，2012.
[68] William J，Emrich J. Nuclear thermal rocket element environmental simulator（NTREES）upgrade activities[C]//Nuclear and Emerging Technologies for Space 2014. Slidell，USA：[s.n.]，2014.
[69] Gerrish H P. Current ground test options for nuclear thermal propulsion[C]//Nuclear and Emerging Technologies for Space 2014. Slidell，USA：[s.n.]，2014.
[70] Stewart M，Schnitzler B G. Multidisciplinary simulation of graphite-composite and cermet fuel elements for NTP point of departure designs[R]. Cleveland，USA：NASA Glenn research Center，2015.
[71] Houts M G，Mitchell D P，Kim T，et al. NASA’s nuclear thermal propulsion project[C]//SPACE Conference & amp. Pasadena，USA：[s.n.]，2015
[72] Borowski S K，Sefcik R J，Fittje J E，et al. Affordable development and demonstration of a small NTR engine and stage：how small is big enough[C]//Space 2015 forum & Exposition. Pasadena，USA：[s.n.]，2015.
[73] Borowski S K，Sefcik R J，Fittje J E，et al. Affordable development and demonstration of a small NTR engine and stage：A preliminary NASA，DOE and Industry assessment[C]//AIAA/ SAE/ASEE 51st Joint Propulsion Conference. Orlando，USA：AIAA，2015
[74] Nikolai N P. Russian space nuclear power and nuclear thermal propulsion systems [J]. Nuclear News,2000,43(13):37-46
[75] 科罗捷耶夫. 核火箭发动机[M]. 郑官庆，王江，黄丽华，译. 北京：中国原子能科学研究院，2005：132-177.
[76] Zakirov V,Pavshook V. Russian nuclear rocket engine design for Mars exploration[J]. Tsinghua Science and Technology,2007,12(3):256-260
[77] Anghaie S. Nuclear thermal propulsion – fuels[R]. Russia：FSUE SRI SIA <Luch>，2006.
[78] Ponomarev-Stepnoy N N，Ranchuk V S，Smetannikov V P. Space nuclear power and propulsion plants based on solid core nuclear reactor with external power conversion unit[C]//Nuclear Energy in Space-2005. Russia：[s.n.]，2005.
[79] 许春阳. 俄罗斯计划开发兆瓦级核火箭发动机[J]. 研究堆与核动力,2010(4):1-6.
[80] Zakirov V,Pavshook V. Feasibility of the recent Russian nuclear electric propulsion concept:2010[J]. Nuclear Engineering and Design,2011,241(5):1529-1537
[81] 邬国伟.核反应堆工程设计[M]. 北京：原子能出版社，1997.
[82] 何伟锋,向红军,蔡国飙. 核火箭原理、发展及应用[J]. 火箭推进,2005,31(2):37-43
He W F,Xiang H J,Cai G B. The fundamentals,developments and applications of nuclear rocket propulsion [J]. Journal of Rocket Propulsion,2005,31(2):37-43
[83] 苏著亭. 核热推进工作原理及应用分析[R]. 北京：中国原子能科学研究院，2003.
[84] 孙征，苏著亭. 14kN核热推进反应堆方案研究[R]. 北京：中国原子能科学研究院，2005.
[85] 解家春,赵守智,贾宝山. SNRE堆芯物理计算分析[J]. 核动力工程,2010,31(5):134-138
Xie J C,Zhao S Z,Jia B S. Core physics calculation and analysis for SNRE[J]. Nuclear Power Engineering,2010,31(5):134-138
[86] 解家春. 载人登陆火星用核热推进系统方案研究[R]. 北京：中国原子能科学研究院，2010.
[87] 霍红磊,安伟健,解家春,等. CERMET-SNRE堆芯物理计算分析[J]. 原子能科学技术,2016,50(12):2150-2156
Huo H L,An W J,Xie J C,et al. Core physics calculation and analysis for CERMET-SNRE[J]. Atomic energy science and technology,2016,50(12):2150-2156
[88] 孙薇.CANP-1堆芯热工水力分析[D].北京：中国原子能科学研究院，2010.
Sun W. Thermal-Hydraulic analysis of CANP-1 reactor core[D]. Beijing：China Institute of AtomicEnergy，2010.
[89] 刘忠恕. 核热火箭发动机系统方案研究[D]. 北京：中国航天科技集团，2017.
Liu Z S. Research on the system of nuclear thermal rocket engine[D]. Beijing：China Aerospace Science and Technology Corporation，2017.
