DEPENDENCE OF BURNING RATE OF A COMPOSITE PROPELLANT ON CHEMICAL STRUCTURE OF FUEL

被引：0
|
作者：
ROMODANO.LD
PEPEKIN, VI
APIN, AY
POKHIL, PF
机构：
来源：
COMBUSTION EXPLOSION AND SHOCK WAVES | 1970年 / 6卷 / 04期
关键词：
D O I：
暂无
中图分类号：
O414.1 [热力学];
学科分类号：
摘要：
引用
收藏
页码：365 / 369
页数：5
相关论文
共 50 条
  • [21] Effect of aluminum particle size on agglomeration size and burning rate of composite propellant
    Fukuchi, Apollo B.
    JOURNAL OF THERMAL SCIENCE AND TECHNOLOGY, 2022, 17 (01):
  • [22] SCALE-UP EFFECTS OF NANOPARTICLE PRODUCTION ON THE BURNING RATE OF COMPOSITE PROPELLANT
    Kreitz, Kevin
    Petersen, Eric
    Reid, David
    Seal, Sudipta
    COMBUSTION SCIENCE AND TECHNOLOGY, 2012, 184 (06) : 750 - 766
  • [23] Computational analysis on burning rate change of composite propellant under tensile strain
    Hu, Song-Qi
    Chen, Jing
    Deng, Zhe
    Liu, Ying-Ji
    Guti Huojian Jishu/Journal of Solid Rocket Technology, 2014, 37 (05): : 672 - 677
  • [24] THE MECHANISM OF BURNING RATE CATALYSIS IN COMPOSITE HTPB-AP PROPELLANT COMBUSTION
    FONG, CW
    HAMSHERE, BL
    COMBUSTION AND FLAME, 1986, 65 (01) : 61 - 69
  • [25] An alternative approach to improve burning rate characteristics and processing parameters of composite propellant
    Sangtyani, Rekha
    Saha, Himadri S.
    Kumar, Amit
    Kumar, Arvind
    Gupta, Manoj
    Chavan, Prakash V.
    COMBUSTION AND FLAME, 2019, 209 : 357 - 362
  • [26] Ignition and combustion characteristics of very high burning rate composite propellant charges
    Shibata, Akio
    Miyake, Atsumi
    Ogawa, Terushige
    Kayaku Gakkaishi/Journal of the Japan Explosives Society, 2000, 61 (02): : 85 - 93
  • [27] Investigation on the propellant burning rate prediction of solid propellant motor
    42nd Inst of the Fourth Acad of CASC, Hubei, China
    Guti Houjian Jishu, 4 (36-40):
  • [28] Effect of nitramine on energy and burning rate of low burning rate HTPB propellant
    Lu, G.
    Guti Huojian Jishu/Journal of Solid Rocket Technology, 2001, 24 (02): : 45 - 47
  • [29] Allowances control of the burning rate of medium burning-rate HTPB propellant
    Guti Houjian Jishu, 2 (35):
  • [30] Calculation of pressure in a solid-propellant rocket motor with the use of a real dependence of the solid propellant burning rate on pressure
    Lipanov, A. M.
    COMBUSTION EXPLOSION AND SHOCK WAVES, 2017, 53 (05) : 569 - 573
12345