Insensitive munitions (IM) and combustion characteristics of GAP/AN composite propellants

被引:16
|
作者
Oyumi, Y
Kimura, E
Hayakawa, S
Nakashita, G
Kato, K
机构
[1] Japan Def Agcy, Tech Res & Dev Inst, Res Ctr 3, Tokyo 190, Japan
[2] NOF Corp, Aichi Works Taketoyo Plant, Dept Res & Dev, Propellant Dev, Aichi 47023, Japan
关键词
D O I
10.1002/prep.19960210511
中图分类号
O69 [应用化学];
学科分类号
081704 ;
摘要
Sensitivities to the ballistic shock and burn rate characteristics of GAP/AN composite propellants were investigated. Nitrate esters, such as TMETN and NC, were very effective ballistic modifier that provided useable burn rate and pressure rate exponent for minimum signature propellant based on AN. Their low temperature mechanical properties become less sensitive to the temperature,, with nitrate esters. Dioctyl adipate platicized propellant showed excellent mechanical properties at operational temperature range.,;. The primary initiation mechanism of card gap test was not dominated by the mechanical properties. Although NC signifcantly increased the critical shock pressure, 14.8% HM and AP were less effective to the sensitivities. GAP/AN propellants showed excellent IM characteristics to die ballistic shock applied here.
引用
收藏
页码:271 / 275
页数:5
相关论文
共 50 条
  • [1] IM characteristics of GAP/AN composite propellants
    TRDI, Japan Defense Agency, Tokyo, Japan
    Kayaku Gakkaishi/Journal of the Japan Explosives Society, 1996, 57 (01): : 9 - 13
  • [3] The transition to insensitive munitions (IM)
    Isler, J
    PROPELLANTS EXPLOSIVES PYROTECHNICS, 1998, 23 (06) : 283 - 291
  • [4] Insensitive Munitions(IM): A Key Aspect of Improved Munitions Safety
    Duncan Watt
    Eric Deschambault
    Patrick Touze
    含能材料, 2006, (05) : 323 - 329
  • [5] Insensitive munitions (IM): A key aspect of improved munitions safety
    Munitions Safety Information Analysis Center , NATO HQ, Brussels, 5-1110, Belgium
    Hanneng Cailiao, 2006, 5 (323-329):
  • [6] Combustion characteristics of GAP based composite propellants (III) - heat release process and burning rate
    Takizuka, Michinori
    Aoki, Ichiro
    2000, Japan Explosives Society, Tokyo, Japan (61):
  • [7] Combustion Behavior of Aluminum Particles in ADN/GAP Composite Propellants
    Weiser, Volker
    Franzin, Andrea
    DeLuca, Luigi T.
    Fischer, Sebastian
    Gettwert, Volker
    Kelzenberg, Stefan
    Knapp, Sebastian
    Raab, Angelika
    Roth, Evelin
    Eisenreich, Norbert
    CHEMICAL ROCKET PROPULSION: A COMPREHENSIVE SURVEY OF ENERGETIC MATERIALS, 2017, : 253 - 270
  • [8] Combustion characteristics of coated nano aluminum in composite propellants
    Sun, Yunlan
    Li, Shufen
    DEFENCE SCIENCE JOURNAL, 2006, 56 (04) : 543 - 550
  • [9] COMBUSTION CHARACTERISTICS OF PHENOL-FORMALDEHYDE COMPOSITE PROPELLANTS
    GIRDHAR, HL
    ARORA, AJ
    INDIAN JOURNAL OF TECHNOLOGY, 1979, 17 (07): : 279 - 280
  • [10] Energy and Combustion Characteristics of Propellants Based on BAMO-GAP Copolymer
    Pei, Jiangfeng
    Zhao, Fengqi
    Wang, Ying
    Xu, Siyu
    Song, Xiuduo
    Chen, Xueli
    CHEMICAL ROCKET PROPULSION: A COMPREHENSIVE SURVEY OF ENERGETIC MATERIALS, 2017, : 341 - 363