常温绿色过氧化氢动力技术现状及发展趋势

单继宏; 王晓东; 张 涛

doi:10.11993/j.issn.2096-3920.2021.06.004

常温绿色过氧化氢动力技术现状及发展趋势

doi: 10.11993/j.issn.2096-3920.2021.06.004

中国科学院催化材料重点实验室大连化学物理研究所, 辽宁大连, 116023

详细信息

作者简介:
单继宏(1973-), 男, 硕士, 正高级工程师, 主要研究方向为绿色推进技术.

中图分类号: TJ630.32
计量
- 文章访问数: 247
- HTML全文浏览量: 23
- PDF下载量: 87
- 被引次数: 0
出版历程
- 收稿日期: 2021-10-21
- 修回日期: 2021-11-05
- 刊出日期: 2021-12-31

Current State and Development Trend of Non-Cryogenic Green Hydrogen Peroxide Power Technology

Dalian Institute of Chemical Physics, State Key Laboratory of Catalysis, Chinese Academy of Sciences, Dalian 116023, China

摘要

摘要: 过氧化氢是常温绿色推进剂的典型代表。文中针对装备动力无毒化、多任务和高效能等使命需求, 概述了过氧化氢本征及其动力技术的特点, 分析了当前美国、欧洲等过氧化氢动力技术的技术状态和发展趋势, 总结了我国自“十五”以来过氧化氢动力技术的发展历程。结合先进空天组合动力、新型固-液混合动力以及重复使用液-液火箭动力等新兴技术发展方向, 介绍了过氧化氢在先进动力研究方面取得的突破, 阐述了催化分解和凝胶赋形等过氧化氢动力关键技术获得的进展和存在的问题。
- 过氧化氢 /
- 组合动力 /
- 固液混合动力
Abstract: Hydrogen peroxide is a typical non-cryogenic green propellant. This paper outlines the intrinsic characteristics of hydrogen peroxide and the characteristics of its power technology for the mission requirements of equipment power nontoxicity, multi-tasking, and high efficiency, analyzes the current technical status and development trend of hydrogen peroxide power technology in Europe and America, and summarizes the development of hydrogen peroxide power technology in China since the “10th Five-Year Plan”. Combined with the advanced aerospace combined power, new solid-liquid hybrid power, reusable liquid-liquid rocket power, and other emerging technology development directions, this paper presents a breakthrough in the research of advanced power of hydrogen peroxide, and expounds the progress and existing problems of key hydrogen peroxide power technologies such as catalytic decomposition and gelation
- hydrogen peroxide /
- combined power /
- solid-liquid hybrid power

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参考文献(30)

[1]	Rocketdyne. North American Aviation. Hydrogen Peroxide Handbook[M]. AFRPL-TR-67-144, 1967.
[2]	Spacecraft Flight Control Systems[M]. Belleville NJ: Walter Kidde & Company, Inc., 1965.
[3]	方懿. 碧海惊雷(下)——美国海军鱼雷发展简史[J]. 国际展望, 2006(6): 78-83.
[4]	Ventura M, Mullens P. The Use of Hydrogen Peroxide for Propulsion and Power[C]//35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Los Angeles, California, USA: AIAA, 1999.
[5]	Toussaint M, Cesco N, Masson F, et al. Development Status of the 200N H2O2 Thruster for aA5-ME Upper Stage Reaction Control System[C]//Space Propulsion Conference. Germany: Cologne, 2014.
[6]	Wernimont E J, Ventura M C. Review of US Historical Rocket Propellants: Accidents, Mishaps & Fatalities[C]// 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Cincinnati, OH, USA: AIAA, 2007.
[7]	Paul Y K, Annik M, Charles P, et al. Design and Development Testing of the TR108-A30Klbf-Thrust-Class Hydrogen Peroxide/Hydrocarbon Pump-Fed Engine[C]//41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Tucson AZ, USA: AIAA, 2005.
[8]	Quinn J E. Oxidizer Selection for the Istar Program (Liquid Oxygen Versus Hydrogen Peroxide)[C]//38th AIAA/ ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Indianapolis, Indiana: AIAA, 2002.
[9]	Siebenhaar A, Bogar T J. Integration and Vehicle Performance Assessment of the Aerojet “Trijet” Combined-Cycle Engine[C]//16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. Bremen, Germany: AIAA, 2009.
[10]	Rhodes B L, Ulrich E R, Hsu A G, et al. Thrust Measurement of a Hydrogen Peroxide Vapor Propulsion System[C]//AIAA Propulsion and Energy Forum. USA: AIAA, 2020.
[11]	Nucleus Completes Successful First Launch, URL[EB/ OL].[2021-08-30].https://www.mynewsdesk.com/no/nammo/pressreleases/nucleus-completes-successful-first-laun-ch-2721547.
[12]	Nammo Signs its Largest Ever Space Development Contract,URL[EB/OL]. [2021-08-30]. https://www.Mynews-desk.com/no/nammo/pressreleases/nammo-signs-its-large-st-ever-space-development-contract-2854799.
[13]	Ruffin A, Fagherazzi M, Bellomo N, et al. Development of the Propulsion System for A Moon Drone Vehicle Demonstrator[C]//AIAA Propulsion and Energy Forum. Reston VA, USA: AIAA, 2021.
[14]	凌前程, 林革, 刘志让. 过氧化氢/煤油双组元推力室催化分解点火研究[J]. 火箭推进, 2003, 29(6): 1-6. Ling Qian-cheng, Lin Ge, Liu Zhi-rang. Investigation on Ignition of the Catalytic Decomposition of H2O2/Kerosene Bipropellant Thruster[J]. Journal of Rocket Propulsion, 2003, 29(6): 1-6.
[15]	李强, 王菊金. 补燃循环过氧化氢/煤油发动机性能敏感性分析[J]. 火箭推进, 2013, 39(5): 35-40. Li Qiang, Wang Ju-jin. Analysis of Performance Sensitivity of Hydrogen Peroxide/kerosene Staged-combustion Engine [J]. Journal of Rocket Propulsion, 2013, 39(5): 35-40.
[16]	白云峰, 林庆国, 金盛宇, 等. 过氧化氢单元催化分解火箭发动机研究[J]. 火箭推进, 2006, 32(4): 15-20. Bai Yun-feng, Lin Qing-guo, Jin Sheng-yu, et al. Rese- arch on Rocket Engine Using Hydrogen Peroxide of Catalytic Decomposition[J]. Journal of Rocket Propulsion, 2006, 32(4): 15-20.
[17]	刘景华, 谭建国, 杨涛, 等. 部分催化过氧化氢变推力发动机的稳定性分析[J]. 航空动力学报, 2007, 22(11): 1954-1957. Liu Jing-hua, Tan Jian-guo, Yang tao, et al. Stability Analysis on Variable Thrust Engine of Partially Catalyzed Hydrogen Peroxide[J]. Journal of Aerospace Power, 2007, 22(11): 1954-1957.
[18]	凌前程. 过氧化氢双组元发动机推力室研究[J]. 火箭推进, 2009, 35(4): 21-25. Ling Qian-cheng. Investigation on Thrust Chamber of the Hydrogen Peroxide Bipropellant Engine[J]. Journal of Rocket Propulsion, 2009, 35(4): 21-25.
[19]	王伟光, 陈晖, 陈炜, 等. 补燃循环先进上面级过氧化氢/煤油涡轮泵研制[J]. 火箭推进, 2016, 42(2): 1-6. Wang Wei-guang, Chen Hui, Chen Wei, et al. Development of a Peroxide/kerosene Turbopump for Afterburning Cycle for Advanced Upper Stage Engine[J]. Journal of Rocket Propulsion, 2016, 42(2): 1-6.
[20]	田含晶, 张涛, 杨黄河, 等. 用于过氧化氢分解的锰铅复合氧化物催化剂[J]. 催化学报, 2000, 21(6): 600-602. Tian Han-jing, Zhang Tao, Yang Huang-he, et al. Manganese-Lead Mixed Oxide Catalysts for Decomposition of Hydrogen Peroxide[J]. Chinese Journal of Catalysis, 2000, 21(6): 600-602.
[21]	吴春田, 王晓东, 周秀楠, 等. 高浓度过氧化氢分解用MnOx/CeO2-Al2O3整体催化剂[J]. 含能材料, 2014, 22 (2): 148-154. Wu Chun-tian, Wang Xiao-dong, Zhou Xiu-nan, et al. MnOx/CeO2-Al2O3 Monolith Catalyst for High Concentration Hydrogen Peroxide Decomposition[J]. Chinese Journal of Energetic Materials, 2014, 22(2): 148-154. [22] 雷娟萍, 林革. 小型化高床载过氧化氢整体式催化剂床研究[J]. 火箭推进, 2008, 34(4): 12-16.
[22]	Lei Juan-ping, Lin Ge. Small High-flux Hydrogen Peroxide Integrated Catalyst Bed[J]. Journal of Rocket Propulsion, 2008, 34(4): 12-16.
[23]	葛明龙, 李强, 刘业奎. 银网催化床分解过氧化氢的计算方法[J]. 火箭推进, 2009, 35(5): 39-45. Ge Ming-long, Li Qiang, Liu Ye-kui. A Calculation Method of Decomposing Hydrogen Peroxide from Silver Catalyst Bed[J]. Journal of Rocket Propulsion, 2009, 35(5): 39-45.
[24]	周志江, 王晓东, 单继宏, 等. 预处理条件对高浓度过氧化氢分解用银网催化剂初始活性的影响[J]. 催化学报, 2006, 27(11): 957-960. Zhou Zhi-jiang, Wang Xiao-dong, Shan Ji-hong, et al. Effect of Pretreatment Conditions on Initial Catalytic Activity of Silver Screen Catalyst for the Catalytic Decomposition of Highly Concentrated Hydrogen Peroxide[J]. Chinese Journal of Catalysis, 2006, 27(11): 957-960.
[25]	韩兆鹏, 郭晟, 刘亚冰, 等. 组合动力用过氧化氢煤油推力室热防护方案设计方法[J]. 推进技术, 2021, 42(10): 2267-2276. Han Zhao-peng, Guo Sheng, Liu Ya-bing, et al. Design Methodology for Thermal Protection of Hydrogen Peroxide and Kerosene Thrust Chamber Used by Combined Cycle Engine[J]. Journal of Propulsion Technology, 2021, 42(10): 2267-2276.
[26]	蔡国飙, 李心瞳, 张源俊. 电动泵压式火箭发动机总体方案设计[C]//第五届空天动力联合会议暨中国航天第三专业信息网第41届技术交流会. 南京: 中国航天科工集团3院31研究所, 2020.
[27]	何渊博, 秦飞, 潘宏亮, 等. 过氧化氢电动泵结构设计与分析[J]. 固体火箭技术, 2021, 44(2): 241-246. He Yuan-bo, Qin Fei, Pan Hong-liang, et al. Structural Design and Analysis of Hydrogen Peroxide Electric Pump [J]. Journal of Solid Rocket Technology, 2021, 44(2): 241-246.
[28]	查志武, 史小锋, 钱志博. 鱼雷热动力技术[M]. 北京: 国防工业出版社, 2006.
[29]	Ventura M C. Long Term Storability of Hydrogen Peroxide[C]//41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Tucson AZ, USA: AIAA, 2005.
[30]	Ventura M, Wernimont E. Advancements in High Concentration Hydrogen Peroxide Catalyst Beds[C]// AIAA-0103250, 37th AIAA Joint Propulsion Conference. Salt Lake City, USA: AIAA, 2001.