可控固体推进技术研究进展

doi:10.13675/j.cnki.tjjs.190449

推进技术 ›› 2020, Vol. 41 ›› Issue (5): 961-973.DOI: 10.13675/j.cnki.tjjs.190449

• 综述 • 下一篇

可控固体推进技术研究进展

鲍立荣^1,2，陈永义^1,2，陈苏杭^1,2，张伟^1,2,3，吴立志^1,2，沈瑞琪^1,2，叶迎华^1,2

1.南京理工大学化工学院，江苏南京 210094;2.南京理工大学空间推进技术研究所，江苏南京 210094;3.南京理工大学特种能源材料教育部重点实验室，江苏南京 210094

发布日期:2021-08-15
作者简介:鲍立荣，硕士生，研究领域为电化学推进技术。E-mail：blr1216@njust.edu.cn
基金资助:
中央高校基本科研业务专项（30919012102；30919011404；30918011315）；特种能源材料教育部重点实验室开放基金（2019SEM08）。

Research Progress on Controllable Solid Propulsion

1.School of Chemical Engineering,Nanjing University of Science and Technology,Nanjing 210094,China;2.Institute of Space Propulsion,Nanjing University of Science and Technology,Nanjing 210094,China;3.Key Laboratory of Special Energy Materials,Ministry of Education，Nanjing University of Science and Technology,Nanjing 210094,China

Published:2021-08-15

摘要/Abstract

摘要： 可控固体推进技术是指在基于含能材料为工质的固体推进剂燃烧过程中，借助一定措施使得推进剂的燃烧方式可控，燃速可调，实现推力可随机控制的推进技术。其可对推进剂燃烧状态进行主动控制，有望从根本上解决固体推进剂发动机推力主动、随机控制等关键技术难题。从推力可控实施方案、对应推进剂类别以及其应用技术等方面对当前可控固体推进技术研究进展进行了综述，并对部分可控固体推进技术中的推力可控实施方案提出了建议。

关键词: 可控固体推进;燃速可调;推力可控;研究进展;综述

Abstract: Controllable solid propulsion refers to the propulsion technology which can control the combustion mode, adjust the burning rate and realize the random control of thrust in the combustion process of solid propellant based on energetic materials. It can actively control the combustion state of propellant, and it is hopeful to fundamentally solve the key technical problems of active and random thrust control of solid propellant motor. The controllable solid propulsion technology was introduced comprehensively from the thrust controllable implementation scheme, the corresponding propellant category and its application technology. And some suggestions on thrust controllable implementation scheme of controllable solid propulsion technology were put forward.

Key words: Controllable solid propulsion;Adjustable burning rate;Controllable thrust;Research progress;Review

鲍立荣，陈永义，陈苏杭，张伟，吴立志，沈瑞琪，叶迎华. 可控固体推进技术研究进展[J]. 推进技术, 2020, 41(5): 961-973.

BAO Li-rong^1,2, CHEN Yong-yi^1,2, CHEN Su-hang^1,2, ZHANG Wei^1,2,3, WU Li-zhi^1,2, SHEN Rui-qi^1,2, YE Ying-hua^1,2. Research Progress on Controllable Solid Propulsion[J]. Journal of Propulsion Technology, 2020, 41(5): 961-973.

参考文献

[1] 于建国, 郑咏岚. 变推力固体火箭发动机战术导弹弹道优化研究[J]. 现代防御技术， 2014， 42(4): 20-23.
[2] Bandyopadhyay S， Subramanian G P， Foust R， et al. A Review of Impending Small Satellite Formation Flying Missions[C]. Florida: 53rd AIAA Aerospace Sciences Meeting， 2015.
[3] 张淑慧，胡波，孟雅桃. 推力可控固体火箭发动机应用及发展[J]. 固体火箭技术， 2002， 25(4): 12-15.
[4] Tahsini A， Farshchi M. Thrust Termination Dynamics of Solid Propellant Rocket Motors[J]. Journal of Propulsion and Power， 2007， 23(5): 1141-1143.
[5] Lewis Jr D H， Janson S W， Cohen R B， et al. Digital Micropropulsion[J]. Sensors and Actuators A: Physical， 2000， 80(2): 143-154.
[6] Rossi C， Scheid E， Esteve D. Theoretical and Experimental Study of Silicon Micromachined Microheater with Dielectric Stacked Membranes[J]. Sensors and Actuators A: Physical， 1997， 63(3): 183-189.
[7] Rossi C， Zhang K， Esteve D， et al. Nanoenergetic Materials for MEMS: a Review[J]. Journal of Microelectromechanical Systems， 2007， 16(4): 919-931.
[8] Lee J， Kim T. MEMS Solid Propellant Thruster Array with Micro Membrane Igniter[J]. Sensors and Actuators A: Physical， 2013， 190: 52-60.
[9] Zhang K L， Chou S K， Ang S S. Development of a Solid Propellant Microthruster with Chamber and Nozzle Etched on a Wafer Surface[J]. Journal of Micromechanics and Microengineering， 2004， 14(6): 785-792.
[10] Sathiyanathan K， Lee R， Chesser H， et al. Solid Propellant Microthruster Design for Nanosatellite Applications[J]. Journal of Propulsion and Power， 2011， 27(6): 1288-1294.
[11] Tanaka S， Kondo K， Habu H， et al. Test of B/Ti Multilayer Reactive Igniters for a Micro Solid Rocket Array Thruster[J]. Sensors and Actuators A: Physical， 2008， 144(2): 361-366.
[12] Puchades I， Hobosyan M， Fuller L F， et al. MEMS Microthrusters with Nanoenergetic Solid Propellants[C]. Toronto: 14th IEEE International Conference on Nanotechnology， 2015.
[13] 汝承博，王飞，许建兵，等. 静电喷射纳米铝热剂的微推进性能[J]. 含能材料， 2016， 24(12): 1136-1144.
[14] Ru C， Fei W， Xu J， et al. Superior Performance of a MEMS-Based Solid Propellant Microthruster (SPM) Array with Nanothermites[J]. Microsystem Technologies， 2017， 23(8): 3161-3174.
[15] Dai J， Wang F， Ru C， et al. Ammonium Perchlorate as an Effective Additive for Enhancing the Combustion and Propulsion Performance of Al/CuO Nanothermites[J]. The Journal of Physical Chemistry C， 2018， 122(18): 10240-10247.
[16] Fricke H D， Burr J W， Sobienick M G. Fluidized Powders-a New Approach to Storable Missile Fuels[C]. Las Vegas: 12th JANNAF Liquid Propulsion Meeting， 1970.
[17] Wickman J. Insitu Mars Rocket and Jet Engines Burning Carbon Dioxide[C]. Los Angeles: 35th Joint Propulsion Conference and Exhibit， 1999.
[18] Shafirovich E， Varma A. Metal-CO₂ Propulsion for Mars Missions: Current Status and Opportunities[J]. Journal of Propulsion and Power， 2008， 24(3): 385-394.
[19] 张胜敏，杨玉新，胡春波. 粉末火箭发动机推力调节试验研究[J]. 固体火箭技术， 2015， 38(3): 347-350.
[20] Loftus H， Montanino L， Bryndle R. Powder Rocket Feasibility Evaluation[C]. New Orleans: 8th Joint Propulsion Specialist Conference， 1972.
[21] Li Y， Hu C， Deng Z， et al. Experimental Study on Multiple-Pulse Performance Characteristics of Ammonium Perchlorate/Aluminum Powder Rocket Motor[J]. Acta Astronautica， 2017， 133: 455-466.
[22] Foote J， Litchford R. Powdered Magnesium-Carbon Dioxide Combustion for Mars Propulsion[R]. AIAA 2005-4469.
[23] Sun H， Hu C， Zhang T， et al. Experimental Investigation on Mass Flow Rate Measurements and Feeding Characteristics of Powder at High Pressure[J]. Applied Thermal Engineering， 2016， 102: 30-37.
[24] Varghese T L， Gaindhar S C， David J， et al. Developmental Studies on Metallised UDMH and Kerosene Gels[J]. Defence Science Journal， 1995， 45(1): 25-30.
[25] Starkovich J， Palaszewski B. Technology for Gelled Liquid Cryogenic Propellants-Metallized Hydrogen/Aluminum[C]. Monterey: 29th Joint Propulsion Conference and Exhibit， 1993.
[26] 陈志刚，杨荣杰. 金属化凝胶推进剂的性能评估[J]. 推进技术， 1998， 19(1): 102-106. (CHEN Zhi-gang， YANG Rong-jie. Performance Evaluation of Metallized Gelled Propellants[J]. Journal of Propulsion Technology， 1998， 19(1): 102-106.)
[27] Zurawski R， Green J. An Evaluation of Metallized Propellants Based on Vehicle Performance[C]. San Diego: 23rd Joint Propulsion Conference， 1987.
[28] Palaszewski B， Powell R. Launch Vehicle Performance Using Metallized Propellants[J]. Journal of Propulsion and Power， 1994， 10(6): 828-833.
[29] Ciezki H K， Naumann K W， Weiser V. Status of Gel Propulsion in the Year 2010 with a Special View on German Activities[C]. Harnaburg: Deutscher Luft-Und Raumfahrtkongress 2010， 2010.
[30] Ciezki H K， Naumann K W. Some Aspects on Safety and Environmental Impact of the German Green Gel Propulsion Technology[J]. Propellants， Explosives， Pyrotechnics， 2016， 41(3): 539-547.
[31] Ciezki H K， Hürttlen J， Naumann K W， et al. Overview of the German Gel Propulsion Technology Program[R]. AIAA 2014-3794.
[32] 宋明德，叶定友，吴心平. 膏体推进剂脉冲火箭发动机新方案的理论和实验研究[J]. 推进技术， 1999， 20(1): 1-5. (SONG Ming-de， YE Ding-you， WU Xin-ping. Theoretical and Experimental Study on a New Scheme of Paste Propellant Pulse Rocket Engine[J]. Journal of Propulsion Technology， 1999， 20(1): 1-5.)
[33] 肖金武，张文刚. PEPA/AP膏体推进剂配方研究[J]. 固体火箭技术， 2001， 24(4): 46-49.
[34] 张明信，张胜勇. 膏体推进剂点火和燃烧特性的实验研究[J]. 固体火箭技术， 2003， 26(2): 30-32.
[35] 张胜勇，毛根旺. 膏体推进剂流动特性实验研究[J]. 固体火箭技术， 2009， 32(5): 521-523.
[36] Petersen E L， Seal S， Stephens M， et al. Self-Extinguishable Solid Propellant[P]. US:413269， 2012-02-14.
[37] Petersen E L， Seal S， Stephens M， et al. Solid Propellant Rocket Motor Having Self-Extinguishing Propellant Grain and Systems Therefrom[P]. US:413284， 2012-12-25.
[38] 高红旭，王瑛，赵凤起. 自熄火固体推进剂的燃烧性能[C]. 大连：中国化学会第30届学术年会， 2016.
[39] Gimelshein N E， Gimelshein S F， Ketsdever A. Thrust Augmentation in Solid Rocket Motors Using Beamed Microwave Energy[R]. AIAA 2009-4962.
[40] Oda Y， Shibata T， Komurasaki K， et al. Thrust Performance of Microwave Rocket under Repetitive-Pulse Operation[J]. Journal of Propulsion and Power， 2009， 25(1): 118-122.
[41] Cornella B， Ketsdever A， Gimelshein N E， et al. Thrust Augmentation of Solid Rocket Motors Using Beamed Microwave Energy[J]. Journal of Propulsion and Power， 2010， 26(5): 1016-1024.
[42] Barkley S J， Zhu K， Lynch J E， et al. Microwave Plasma Enhancement of Multiphase Flames: On-Demand Control of Solid Propellant Burning Rate[J]. Combustion and Flame， 2019， 199: 14-23.
[43] Dunning J， Sankovic J. NASA's Electric Propulsion Program[R]. AIAA 2005-3145.
[44] Sawka W N， Katzakian Jr A， Grix C. Solid State Digital Propulsion Cluster Thrusters for Small Satellites Using High Performance Electrically Controlled Extinguishable Solid Propellants[C]. Logan: 19th Annual AIAA/USU Conference on Small Satellites， 2005.
[45] Grix C， Sawka W N. Electrically Controlled Extinguishable Solid Propellants: a Safe， Broadly Scalable Propulsion Technology[C]. Monterey: 53rd JANNAF Propulsion Meeting， 2005.
[46] Chung K， Rozumov E， Kaminsky D， et al. Development of Electrically Controlled Energetic Materials (ECEM)[J]. ECS Transactions， 2013， 50(40): 59-66.
[47] Sawka W N， McPherson M. Electrical Solid Propellants: a Safe， Micro to Macro Propulsion Technology[R]. AIAA 2013-4168.
[48] Koehler F， Langhenry M， Summers M， et al. Electric Propellant Solid Rocket Motor Thruster Results Enabling Small Satellites[C]. Logan: 30th Annual AIAA/USU Conference on Small Satellites， 2017.
[49] Summers M H， Villarreal J K， Langhenry M T， et al. Electrode Ignition and Control of Electrically Operated Propellants[P]. US: 197421， 2018-01-04.
[50] 王新强，邓康清，李洪旭，等. 电控固体推进剂点火技术研究[J]. 固体火箭技术， 2017， 40(3): 313-318.
[51] 胡建新，李洋，何志成，等. 电控固体推进剂热分解和燃烧性能研究[J]. 推进技术， 2018， 39(11): 2588-2594.
[52] 鲍立荣，张伟，陈永义，等. HAN基电控固体推进剂的热分解和电导率特性[J]. 含能材料， 2019， 27（9）： 743-748.
[53] Grix C E， Sawka W N. Family of Modifiable High Performance Electrically Controlled Propellants and Explosives[P]. US: 993084， 2014-11-18.
[54] Kakami A， Hamada T， Shimoda M， et al. Throttleable Solid Propellant Microthruster Using Laser-Assisted Combustion[R]. AIAA 2013-4078.
[55] Kakami A， Masaki S， Horisawa H， et al. Solid Propellant Microthruster Using Laser-Assisted Combustion[R]. AIAA 2004-3797.
[56] Kakami A， Hiyamizu R， Shuzenji K， et al. Laser-Assisted Combustion of Solid Propellants[R]. AIAA 2007-5783.
[57] Kakami A， Takai T， Tachibana T. Solid Propellant Combustion under Laser Heating[R]. AIAA 2008-4788.
[58] Isakari S， Asakura T， Haraguchi D， et al. Performance Evaluation and Thermography of Solid-Propellant Microthrusters with Laser-Based Throttling[J]. Aerospace Science and Technology， 2017， 71: 99-108.
[59] Kakami A， Haraguchi D， Matsuura Y， et al. Effect of Carbon Black on Performance of Laser-Controlled Solid Propellant Microthruster[C]. Cincinnati: 2018 Joint Propulsion Conference， 2018.
[60] Shen R， Wu L， Qin Z， et al. New Concept of Laser-Augmented Chemical Propulsion[M]. Berlin: Springer， 2017.
[61] 沈瑞琪，段卜仁，章皓男，等. 燃速可控的光敏推进剂[P]. 中国专利：108373397， 2018-08-07.
[62] Rossi C， Briand D， Dumonteuil M， et al. Matrix of 10×10 Addressed Solid Propellant Microthrusters: Review of the Technologies[J]. Sensors and Actuators A: Physical， 2006， 126(1): 241-252.
[63] Tanaka S， Hosokawa R， Tokudome S， et al. MEMS-Based Solid Propellant Rocket Array Thruster[J]. Transactions of the Japan Society for Aeronautical and Space Sciences， 2003， 46(151): 47-51.
[64] Nicholas A， Finne T， Galysh I， et al. SpinSat Mission Overview[C]. Logan: 27th Annual AIAA/USU Conference on Small Satellites， 2013.
[65] Kakami A， Terashita S， Tachibana T. Application of Laser-Assisted Combustion to Solid Propellant for Space Propulsion[R]. AIAA 2010-6584.
[66] Kakami A， Morita， Taketoshi H， et al. Laser Assisted Combustion of Solid Propellant for a 100mN Class Variable Thrust Rocket Motor[R]. AIAA 2012-4042.
[67] He N， Chen Y， Wu L， et al. Combustion Characteristics of 5-Aminotetrazole-Based Propellant for Laser Hybrid Propulsion[J]. International Journal of Energetic Materials and Chemical Propulsion， 2017， 16(3): 207-218.
[68] Szabo J， Miller T， Herr J， et al. Magnesium Bipropellant Rockets for Martian Ascent Vehicles[R]. AIAA 2011-5834.
[69] 李芳，胡春波，何国强. Mg粉/CO₂粉末火箭发动机性能分析[J]. 固体火箭技术， 2010， 33(4): 414-418.
[70] Wickman J， James E. Gelled Liquid Oxygen/Metal Powder Monopropellants[C]. Nashville: 28th Joint Propulsion Conference and Exhibit， 1992.
[71] Yasuhara W， Olson A， Finato S. Advanced Gel Propulsion Controls for Kill Vehicles[C]. Albuquerque: Annual Interceptor Technology Conference， 1993.
[72] Kukushkin V. State and Prospects of Solid Propellant Rocket Development[C]. Nashville: 28th Joint Propulsion Conference and Exhibit， 1992.
[73] 闫大庆，周宏民，单建胜. 凝胶/膏状推进剂研究发展状况[J]. 火箭推进， 2003， 29(1): 38-46.
[74] Madlener K， Ciezki H， Von Kampen J， et al. Characterization of Various Properties of Gel Fuels with Regard to Propulsion Application[R]. AIAA 2008-4870.
[75] 刘爱华，崔金平，李前虎. 膏体冲压发动机输送及调节技术试验研究[J]. 弹箭与制导学报， 2010， 30(1): 151-152.
[76] 张积炳. 膏体富燃料推进剂冲压发动机挤压输送特性试验研究[J]. 航空兵器， 2010, (4): 62-64.
[77] Chung K， Rozumov E， Kamin-sky D， et al. Development of Electrically Controlled Energetic Materials for 120mm Tank Igniters[C]. Las Vegas: Insensitive Munitions and Energetic Materials Technology Symposium， 2012.
[78] McCauley R， Fischbach S， Fredrick R. Controllable Solid Propulsion Combustion and Acoustic Knowledge Base Improvements[R]. NASA AFP-2012-2457.

可控固体推进技术研究进展

Research Progress on Controllable Solid Propulsion

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