Ignition of Hydrogen Peroxide with Gel Hydrocarbon Fuels

被引:27
作者
Connell, Terrence L., Jr. [1 ]
Risha, Grant A. [2 ]
Yetter, Richard A. [1 ]
Natan, Benveniste [3 ]
机构
[1] Penn State Univ, Dept Mech & Nucl Engn, University Pk, PA 16802 USA
[2] Penn State Univ, Dept Engn, Altoona Coll, University Pk, PA 16802 USA
[3] Technion Israel Inst Technol, Fac Aerosp Engn, IL-32000 Haifa, Israel
关键词
N-HEPTANE; SHOCK-TUBE; DECOMPOSITION; COMBUSTION; PRESSURES; OXIDATION; MIXTURES; DODECANE; NABH4; TIMES;
D O I
10.2514/1.B36458
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Experimental counterflow and impinging jet studies and modeling analysis of hypergolic hydrogen peroxide (H2O2) and gel hydrocarbon fuel/particle mixtures were conducted to characterize condensed phase reaction rates and ignition delay times. The mixtures consisted of n-dodecane, n-heptane, and kerosene containing fumed silica and sodium borohydride (NaBH4) particles. Scanning electron microscopy, x-ray photoelectron spectroscopy, and simultaneous thermogravimetric and differential scanning calorimetry analysis of the NaBH4 particles were performed to characterize particle size, size distribution, geometry, surface composition, and thermal decomposition. Liquid-phase counterflow experiments were used to derive a global rate constant for the condensed phase reaction between H2O2 and NaBH4. Chemical kinetics calculations were performed using the condensed phase global reaction coupled with a detailed gas phase mechanism for hydrocarbon oxidation to phenomenologically study the ignition process. Shorter ignition delays were achieved when fuel flow was established before oxidizer injection. Ignition delay decreased with NaBH4 addition until a limiting loading was achieved, after which ignition delay remained nearly constant. Elevating the reactant temperature reduced ignition delay, consistent with fuel volatility trends. Modeling results show that the ignition process relies upon the reaction between NaBH4 and H2O2 to gasify and heat an ignition kernel to the H2O2/fuel mixture autoignition temperature.
引用
收藏
页码:170 / 181
页数:12
相关论文
共 36 条
  • [1] [Anonymous], 2001, ICT DAT THERM VAL VE
  • [2] HYDROGEN-SENSITIZED DECOMPOSITION OF HYDROGEN PEROXIDE
    BALDWIN, RR
    BRATTAN, D
    TUNNICLI.B
    WALKER, RW
    WEBSTER, SJ
    [J]. COMBUSTION AND FLAME, 1970, 15 (02) : 133 - &
  • [3] Bittner D., 2013, 49 AIAA ASME SAE ASE
  • [4] SHOCK-TUBE INVESTIGATION OF SELF-IGNITION OF N-HEPTANE AIR MIXTURES UNDER ENGINE RELEVANT CONDITIONS
    CIEZKI, HK
    ADOMEIT, G
    [J]. COMBUSTION AND FLAME, 1993, 93 (04) : 421 - 433
  • [5] Propulsive performance of a hypergolic H2O2/kerosene bipropellant
    Cong, Y
    Zhang, T
    Li, T
    Suo, JW
    Wang, XD
    Ma, L
    Liang, DB
    Lin, LW
    [J]. JOURNAL OF PROPULSION AND POWER, 2004, 20 (01) : 83 - 86
  • [6] Connell Jr T. L., P 10 INT S SPEC TOP
  • [7] Connell T. L., 2014, 50 AIAA ASME SAE ASE
  • [8] A comprehensive modeling study of n-heptane oxidation
    Curran, HJ
    Gaffuri, P
    Pitz, WJ
    Westbrook, CK
    [J]. COMBUSTION AND FLAME, 1998, 114 (1-2) : 149 - 177
  • [9] Diede A, 2004, U.S. Patent, Patent No. [6,695,938, 6695938]
  • [10] THE BEHAVIOUR OF MIXTURES OF HYDROGEN PEROXIDE AND WATER .1. DETERMINATION OF THE DENSITIES OF MIXTURES OF HYDROGEN PEROXIDE AND WATER
    EASTON, MF
    MITCHELL, AG
    WYNNEJONES, WFK
    [J]. TRANSACTIONS OF THE FARADAY SOCIETY, 1952, 48 (09): : 796 - 801