Combustion Characteristics of a Hydroxylammonium Nitrate Based Liquid Propellant. Combustion Mechanism and Application to Thrusters (vol 45, pg 442, 2009)

被引：0
|
作者：
Katsumi, T.
Kodama, H.
Matsuo, T.
Ogawa, H.
Tsuboi, N.
Hori, K.
机构：
[1] The Graduate University for Advanced Studies (SOKENDAI),
[2] Mitsubishi Heavy Industries,undefined
[3] Ltd.,undefined
[4] Institute of Space and Astronautical Sciences,undefined
来源：
COMBUSTION EXPLOSION AND SHOCK WAVES | 2009年 / 45卷 / 05期
关键词：
D O I：
10.1007/s10573-009-0077-6
中图分类号：
O414.1 [热力学];
学科分类号：
摘要：
引用
收藏
页码：634 / 634
页数：1
相关论文
共 29 条
  • [1] Combustion characteristics of a hydroxylammonium nitrate based liquid propellant. Combustion mechanism and application to thrusters
    Katsumi, T.
    Kodama, H.
    Matsuo, T.
    Ogawa, H.
    Tsuboi, N.
    Hori, K.
    COMBUSTION EXPLOSION AND SHOCK WAVES, 2009, 45 (04) : 442 - 453
  • [2] Combustion characteristics of a hydroxylammonium nitrate based liquid propellant. Combustion mechanism and application to thrusters
    T. Katsumi
    H. Kodama
    T. Matsuo
    H. Ogawa
    N. Tsuboi
    K. Hori
    Combustion, Explosion, and Shock Waves, 2009, 45 : 442 - 453
  • [3] Erratum to: Combustion Characteristics of a Hydroxylammonium Nitrate Based Liquid Propellant. Combustion Mechanism and Application to Thrusters
    T. Katsumi
    H. Kodama
    T. Matsuo
    H. Ogawa
    N. Tsuboi
    K. Hori
    Combustion, Explosion, and Shock Waves, 2009, 45 : 634 - 634
  • [4] Assessment of combustion characteristics and mechanism of hydroxylammonium nitrate-based liquid monopropellant
    Chang, YP
    Kuo, KK
    JOURNAL OF PROPULSION AND POWER, 2002, 18 (05) : 1076 - 1085
  • [5] Ignition and flow combustion characteristics of hydroxylammonium nitrate- based liquid propellant based on electric method
    Jin, Bao-zhi
    Ma, Jun-qiang
    Li, Guo-xiu
    Li, Hong-meng
    ACTA ASTRONAUTICA, 2024, 224 : 172 - 182
  • [6] HYDROXYLAMMONIUM NITRATE-BASED LIQUID PROPELLANT COMBUSTION - INTERPRETATION OF STRAND BURNER DATA AND THE LAMINAR BURNING VELOCITY
    VOSEN, SR
    COMBUSTION AND FLAME, 1990, 82 (3-4) : 376 - 388
  • [7] Tuning combustion and energy in hydroxylammonium nitrate (HAN)-based electrically controlled solid propellant
    Li, Feng
    Wang, Zhiwen
    Zhang, Qianyi
    Cheng, Zeyu
    Yu, Yixin
    Shen, Ruiqi
    Ye, Yinghua
    Deluca, Luigi T.
    Zhang, Wei
    CHEMICAL ENGINEERING JOURNAL, 2024, 487
  • [8] Combustion characteristics of HAN-based liquid propellant
    Department of Space and Astronautical Science, Graduate University for Advanced Studies , 3-1-1 Yoshinodai, Sagamihara-shi, Kanagawa-ken, 229-8510, Japan
    不详
    不详
    Sci. Technol. Energ. Mater., 2009, 1-2 (27-32):
  • [9] Combustion characteristics of HAN-based liquid propellant
    Katsumi, Toshiyuki
    Kodama, Hiroyuki
    Ogawa, Hiroyuki
    Tsuboi, Nobuyuki
    Hori, Keiichi
    SCIENCE AND TECHNOLOGY OF ENERGETIC MATERIALS, 2009, 70 (1-2) : 27 - 32
  • [10] Combustion Characteristics of a Hydroxylammonium-Nitrate-Based Monopropellant Thruster with Discharge Plasma System
    Wada, Asato
    Watanabe, Hiroki
    Takegahara, Haruki
    JOURNAL OF PROPULSION AND POWER, 2018, 34 (04) : 1052 - 1060
123