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低温固体推进技术基础和研究现状 被引量：1

Fundamentals and research status of cryogenic solid propulsion technology
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摘要 介绍一个新的化学火箭推进领域———低温固体推进技术 ,叙述了这种新一代固体火箭发动机的基本原理、结构形式、特点和有关技术问题 ,近年来国外研究工作取得的进展及应用于航天运载火箭的潜力。 A new category of chemical rocket propulsion-cryogenic solid propulsion technology is presented. The fundamentals, structural configurations,features, technical challenges concerned,recent advances in the research activities in the world and potential merits in application to space launch vehicles are discussed.
作者 张德雄 姚润森
机构地区 中国航天科技集团公司四院四十七所
出处 《固体火箭技术》 EI CAS CSCD 北大核心 2002年第3期8-11,共4页 Journal of Solid Rocket Technology
关键词 低温固体推进技术 研究现状 固体推进剂火箭发动机 低温推进剂 高能推进剂 solid propellant rocket engine cryogenic propellant high energy propellant
分类号 V435 [航空宇航科学与技术—航空宇航推进理论与工程] V512 [航空宇航科学与技术—航空宇航推进理论与工程]
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参考文献9

  • 1[1]Lo R. Advances in cryogenic solid propulsion [ C ]. 31 st Int. Ann. Conf. ICT, June 27-30,2000, Paper V 15.
  • 2[2]Froning Jr H. D. Possible revolutions in rocket propulsion [ R]. IAA-98-IAA,3303.
  • 3[3]Lo R E. Modular dissected cryoenie solid-rocket propellant grains[ C]. IAF-98-S310.
  • 4[4]Lo R E. A novel kind of solid rocket propellant [ J ]. Aerospace Science and Technology, 1998, (6).
  • 5[5]Palaszewski B. Atomic hydrogen propellants: Historical perspectives and future possibilities[ R]. AIAA-93-0244.
  • 6[6]Adirim H. Next generation high performance low pollution launchers: problems and solutions[ R]. IAA-99-IAA3301.
  • 7[7]Carriek P G. Theoretical performance of high energy density cryogenic solid rocket propellants[ R]. AIAA-95-2892.
  • 8[8]Lo R E. Multiple boundary layer hybrid combustion in modular CSP-propellant charges[ R]. AIAA 2001-3536.
  • 9[9]Weiser V. Experiments and modeling to study the burning behavior of cryogenic solid propellant[ R]. AIAA 2001-3856.

同被引文献13

  • 1庞爱民,郑剑.高能固体推进剂技术未来发展展望[J].固体火箭技术,2004,27(4):289-293. 被引量：74
  • 2Patrick G Carrick.Theoretical performance of high energy density cryogenic solid rocket propellant[R].A1995-2892.
  • 3Lo R E.A novel kind of solid rocket propellant[J].Aerospace Science and Technology,1998,2(6):359-367.
  • 4Roger E Lo,Harry Adirim.Recent advances in cryogenic solid propellant multiple hybrid,combustion[C]∥IAC-05-C4.2.01.
  • 5arry Adirim,Roger E Lo,Norbert Pilz,et al.Cryogenic solid propulsion technology development status[C]∥41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference,Tucson,USA,2005.
  • 6Harry Adirim,Roger E Lo,Norbert Pilz.State-of-the-art in cryogenic solid propulsion research[C]∥42nd AIAA ASME/SAE/ASEE Joint Propulsion Conference,California,USA,2006.
  • 7Franson C,Orlandi O,Perut C,et al.New high energetic composite propellants for space applications:Refrigerated Solid Propellant (RSP)[R].http://innerarch.eu/docs/eucassfinal_5_01_04.pdf.
  • 8Roger E.Lo,Harry Adirim,Sascha poller,et al.Advances in green cryogenic solid propellant propulsion[C]∥2nd Int.conference on green propellant for Space propulsion,2004,10:557-564.
  • 9Roger E Lo.Experimental investigation on cryogenic solid propellants in a combustion chamber[C]∥41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference,Tucson,USA,2005.
  • 10Volker Weiser,Norbert Eisenreich,Sascha Poller,et al.Investigation of the burning behavior of cryogenic solid propellants[J].Propellants,Explosives,Pyrotechnics,2002,27:150-155.

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固体火箭技术
2002年 第3期

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