[1]庞维强,王可,胥会祥,等.含碳氢燃料(ACH)的低特征信号富燃料推进剂特性[J].固体火箭技术,2018,41(06):732-739.
 PANG Weiqiang,WANG Ke,XU Huixiang,et al.Performances of low signature fuel rich propellantwith hydrocarbon fuel(ACH)[J].Journal of Solid Rocket Technology,2018,41(06):732-739.
点击复制

含碳氢燃料(ACH)的低特征信号富燃料推进剂特性

参考文献/References:

[1]赵庆华,乌日嘎,刘欣,等.国外低特征信号富燃料推进剂的研究进展[J].化学推进剂与高分子材料,2010,8(6):11-13.ZHAO Qinghua,WU Riga,LIU Xin,et al.Research progress of low signature fuel rich propellants abroad[J].Chemical propellants and polymer materials,2010,8(6):11-13.

[2]Joseph M,Makhlouf,et al.Method of preparing tetraethylammoniumdecahydrodecaborates[P].US 3373202.1968,03.
[3]刘继华.火药物理化学性能[M].北京:北京理工大学出版社,1997.
[4]庞维强,薛云娜,樊学忠,等.十氢十硼酸双四乙基铵的热行为及其与推进剂组分的相容性研究[J].含能材料,2012,20(3):280-285.PANG Weiqiang,XU Yunna,FAN Xuezhong,et al.Thermal Behavior of Tetraethylammonium Dodecahydrododecaborates (BHN) and its Compatibility with Main Components of Propellant[J].Chinese Journal of Energetic Materials,2012,20(3):280-285.
[5]Richard A Yetter,Grant A Risha,Steven F Son.Metal particle combustion and nanotechnology[J].Proceedings of the Combustion Institute,2009,32:1819-1838.
[6]Abdullah Ulas,Kenneth K Kuo,Carl Gotzmer.Ignition and combustion of boron particles in fluorinecontaining environments[J].Combustion and Flame,2001,127:1935-1957.
[7]Pang Weiqiang,Fan Xuezhong,Zhang Wei,et al.Application of amorphous boron granulated with hydroxylterminated polybutadiene in fuel rich solid propellant[J].Propellants,Explosives,Pyrotechnics,2011,36:360-366.
[8]Stephens William D.Fullerene rocket fuels:US,5341639[P].1994.
[9]Meclendon S E,Miller W H,Herty C H.Fuel selection criteria for ducted rocket application[R],AIAA 1980-1120.
[10]Hatcher Richard C,Stephens William D,Stanley Robert L.Solid fuel gas generator for ducted rocket engine:US,6258188[P].2001.
[11]庞维强,樊学忠,赵凤起,等.高能燃烧剂(BHN)对富燃料推进剂特性的影响[J].固体火箭技术,2013,36(5):647-651.PANG Weiqiang,FAN Xuezhong,ZHAO Fengqi,et al.Effects of high energetic combustion agents (BHN) on the properties of fuel rich solid propellant [J].Solid Rocket Technology,2013,36(5):647-651.?
[12]庞维强,樊学忠,胥会祥,等.富燃料固体火箭推进剂技术[M].西安:西北工业大学出版社,2016.
[13]吴雄岗,宋桂贤,严启龙,等.Mg/Al合金对CMDB推进剂燃烧性能的影响[J].推进技术,2012,33(4):597-562.WU Xionggang,SONG Guixian,YAN Qilong,et al.Investigation on the Combustion Behavior of CMDB Propellant with Mg/Al Alloy[J].Journal of Propulsion Technology,2012,33(4):597-562.
[14]Rashkovsky S A.Aluminum agglomeration in composite solid propellant combustion[J].Journal de Pyhsique,2002,12(7):453-458.
[15]单文刚,孙铁刚,张国东.碳硼烷衍生物对固体推进剂燃烧性能影响研究[J].固体火箭技术,1995,18 (3):24-26.SHAN Wengang,SUN Tiegang,ZHANG Guodong.Effects of carborane derivatives on the combustion of solid propellants[J].Solid Rocket Technology,1995,18 (3):24-26.[16]Slobodan M,Vuga.Effects of liquid burn rate catalysts on rheological properties of highenergy composite propellants[J].Propellants,Explosives,Pyrotechnics,1991,16:293-298.

相似文献/References:

[1]高东磊,张炜,朱慧,等.团聚硼对富燃料推进剂燃烧性能的影响[J].固体火箭技术,2008,(2):161.
[2]张君启,张炜,赵凤起,等.含3,4-二氨基呋咱低特征信号富燃料推进剂能量性能及特征信号分析 [J].固体火箭技术,2008,(6):621.
[3]石磊,王英红,陈宏杰,等.多残渣富燃料推进剂燃速测试仪的改进[J].固体火箭技术,2010,(03):360.
[4]陈超,王英红,张放利.铝粉粒径对高铝含量富燃料推进剂一次燃烧性能的影响[J].固体火箭技术,2010,(06):670.
[5]邱俊,何国强,刘佩进,等.富燃料推进剂燃烧产物粒度参数的激光衰减法测量[J].固体火箭技术,2011,(04):533.
[6]庞维强,樊学忠,胥会祥,等.含团聚硼富燃料推进剂表-界面性能研究[J].固体火箭技术,2013,(04):521.
[7]庞维强,樊学忠,赵凤起,等.高能燃烧剂(BHN)对富燃料推进剂特性的影响[J].固体火箭技术,2013,(05):647.

更新日期/Last Update: 2019-01-03
PDF下载 分享