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金属化胶体推进剂性能研究 被引量:2

Performance Rearch of Metallized Gelled Propellant
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摘要 对金属化胶体推进剂的热力学、流变学、燃烧及燃烧效率等的分析研究表明,金属化胶体推进剂性能与金属粉末的添加量和金属半径有关;金属粉末的添加量主要影响液体推进剂的热力学和流变性能;金属粉末颗粒半径大小对推进剂燃烧效率、燃烧速率等性能产生重要影响,金属颗粒半径越小,推进剂燃烧越完全,燃烧效率越高。 The thermodynamics, rheology, combustion of metallized gelled propellants(MGPs) are analysed. It is showed that the performance of MGPs is related to the amount and grain size of metal power added. The amount of metal power affects the thermodynamics and rheology perfence of MGPs.The smaller the grain size of metal power is, the more complete is the combustion and with higer efficiency.
出处 《导弹与航天运载技术》 北大核心 2006年第3期52-55,共4页 Missiles and Space Vehicles
关键词 火箭发动机 胶体 推进剂 Rocket engine Gel Propellant
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参考文献8

  • 1禹天福.胶体推进剂的研究与应用[J].导弹与航天运载技术,2002(5):36-43. 被引量:13
  • 2Rapp D C,Zurawski R L.Characterization of aluminum/RP-1 gel propellant properties[R].AIAA 88-2821.
  • 3Palaszewski B.Metallized gelled propellants:oxygen/RP-1/aluninumrocket engine calorimeter heat transfer measurements analysis[R].AIAA 97-2974.
  • 4Palaszewski B,Zakany J.Metallized gelled propellants:oxygen/rp-1/aluminum rocket heat transfer and combustion experiments[R].AIAA 96-2622.
  • 5Mordosky J W,Zhang B Q,Kuo K K.Spray combustion of gelled RP-1 propellants containing nano-sized aluminum particles in rocket engine conditions[R].AIAA 2001-3274.
  • 6禹天福.偏二甲肼胶体流变学研究[J].火箭推进,2004,30(3):36-41. 被引量:4
  • 7Palaszewski B,Zakany J.Metallized gelled propellants:oxygen/RP-1/Aluminum rocket combustion[R].AIAA 95-2435.
  • 8Galecki D L.Ignition and combustion of metallized propellants[R].AIAA 89-2883.

二级参考文献19

  • 1Cabeal J A et al.System analysis of gelled space-storable propellants.N70-35084,1970.
  • 2Cabeal J A et al.System analysis of space-storable propellants.N70-39629,1970.
  • 3Munjal N L,Gupta B L,Varma Mohan. Preparative and mechanistic studies on unsymmetrical dimethylhydrazine-red fuming nitric acid liquid propellant gels.Propellants,Explosives,Pyrotechnics,1985,10(4):111~117
  • 4Gupta B L et al.Rheological studies on virgin and metallized unsymmetrical dimethylhydrazine gelled systems.Propellant,explosive,pyrotechnics,1986,11:45~52
  • 5Zurawski Robert L et al.An evaluation of metallized propellants based on vehicle performance.AIAA 87-1773,1987.
  • 6Rapp D C et al.Characterization of RP-1/Aluminum gel propellant properties.AIAA 88-2821,1988.
  • 7Rapp D C et al. Propulsion safety almost equals mission safety.AIAA 88-2881,1988.
  • 8Galecki D L.Ignition and combustion of metallized propellants.AIAA 89-2883 ,1989.
  • 9Giola G et al.Advanced gel(agel) technology program. AD/A-216254,1989.
  • 10Palaszewski Bryan A. Upper stages using liquid propulsion and metallized propellants.NASA TP-3191,1990.

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