The Selection of Composite Solid Propellant Process Condition Based on Flow Characteristics of Propellant Slurry

被引:3
|
作者
Abdillah, L. A. [1 ]
Restasari, A. [1 ]
Hartaya, K. [1 ]
Budiman, Y. [1 ]
机构
[1] Natl Inst Aeronaut & Space, Rocket Technol Ctr, Bogor, Indonesia
关键词
D O I
10.1063/5.0002342
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Propellant slurry is kind of non-Newtonian fluid that the characteristics can be affected by process conditions i.e time, temperature, and mixing speed. It is known that composite propellant is made of solid and liquid materials mixed together using a mixer becomes a relatively high-viscosity slurry. Mixing technique of high-viscosity system is challenging because there is no Eddy's turbulence to distribute the components. The suitable technique for this system is laminar mixing technique. Through this technique, it will conduct a research on the propellant slurry's flow characteristics as the mixing time changes. The purpose of this paper was to discover the fluid type and characteristics of propellant slurry that can be used as a reference in selecting the process conditions. The result shows that the propellant slurry behave as shear thinning or pseudoplastic fluid. The optimum process condition that produces good characteristics slurry with values of n = 0.918 and k = 2246.21 dyne.sn/cm2, was at 115 minutes of total mixing time.
引用
收藏
页数:7
相关论文
共 50 条
  • [31] Study on the effect of potassium compound on the combustion characteristics of HTPB composite solid propellant
    Zhao, Yiding
    Liu, Jianzhong
    Gao, Huanhuan
    Xie, Peini
    Liao, Xueqin
    JOURNAL OF THERMAL ANALYSIS AND CALORIMETRY, 2024, 149 (10) : 4469 - 4477
  • [32] The effect of strain rate and temperature on mechanical characteristics of aluminised composite solid propellant
    Kadiresh, P. N.
    Venkatesan, S. P.
    INTERNATIONAL JOURNAL OF AMBIENT ENERGY, 2020, 43 (01) : 2710 - 2713
  • [33] Prediction of Burning Characteristics of Dihydroxyglyoxime Composite Propellant
    Jang, Jesun
    Kwon, Sejin
    JOURNAL OF PROPULSION AND POWER, 2023, 39 (05) : 743 - 753
  • [34] Low strain rate yield characteristics and failure modes of solid composite propellant
    Deng, K. W.
    Li, H. Y.
    Shen, Z. B.
    Zhang, X.
    Weng, J. X.
    ENGINEERING FAILURE ANALYSIS, 2023, 150
  • [35] Safety analysis on truing process of solid propellant
    Li, Jun
    Jiao, Qing-jie
    Ren, Hui
    DEFENCE TECHNOLOGY, 2018, 14 (05): : 612 - 615
  • [36] Safety analysis on truing process of solid propellant
    Jun Li
    Qing-jie Jiao
    Hui Ren
    Defence Technology, 2018, (05) : 612 - 615
  • [37] Erosive burning of a solid propellant in a supersonic flow
    Arkhipov, VA
    Zimin, DA
    COMBUSTION EXPLOSION AND SHOCK WAVES, 1998, 34 (01) : 55 - 57
  • [38] Pipe flow characteristics of pasty propellant based on MAC method
    Shan X.
    Li Y.
    Wu Y.
    Chen X.
    He Y.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2023, 38 (10): : 2430 - 2440
  • [39] Erosive burning of a solid propellant in a supersonic flow
    V. A. Arkhipov
    D. A. Zimin
    Combustion, Explosion and Shock Waves, 1998, 34 : 55 - 57
  • [40] Application of Aluminum-based Composite Fuel in NEPE Solid Propellant
    Wang H.-S.
    Zhang X.
    Wang Y.-W.
    Du F.
    Li L.
    Gu J.
    Li W.
    Tao B.-W.
    Hanneng Cailiao/Chinese Journal of Energetic Materials, 2022, 30 (08): : 819 - 825