High-energy-density metallized gel propellant by hydrogen-bonded polymer-small molecules for enhanced stability and shear-thinning performance

被引:7
作者
Huang, Liya [1 ]
Gong, Mingquan [1 ]
Zhang, Jiarui [1 ]
Liang, Kun [1 ]
Yang, He [1 ]
机构
[1] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Peoples R China
基金
中国国家自然科学基金;
关键词
Metallized gel; Cooperative hydrogen bonding; Mixture design; Rheological properties; Spray combustion; SURFACE-TENSION; FUEL; IGNITION; TEMPERATURE; VISCOSITY; CELLULOSE; SPRAY; BORON;
D O I
10.1016/j.actaastro.2023.10.047
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Metallized gel propellants with high metal content hold significant potential for enhancing the energy properties of hydrocarbon fuels. However, achieving an optimal balance between storage stability and atomization characteristics poses a significant challenge. In this study, we successfully synthesized metallized gel propellants that exhibit exceptional stability and remarkable shear-thinning properties by utilizing cooperative hydrogen bonding between polymer octanoyl cellulose and the small Thixatrol ST molecule. Through meticulous mixture design and formulation optimization, the metallized gel propellants demonstrated noteworthy characteristics, including a high calorific value of 48.48 MJ/kg, an impressive dynamic stability index of 89.12%, a surface tension of 23.21 mN/m, and sustained stability for at least six months under resting conditions. The metallized gel propellant, containing 50 wt% boron particles, exhibited a density 1.54 times higher than pure kerosene, meeting the requirements for enhancing specific impulse in rocket and ramjet engines. Moreover, optimized samples with varying boron concentrations were evaluated for their rheological properties and atomization behavior. The results revealed that the inclusion of boron particles increased the viscosity of the metallized gels. Consequently, the sample with 50 wt% boron exhibited modified viscosity-flow behavior, resulting in the formation of larger gel droplets during atomization. Finally, the metallized gel propellant demonstrated successful ignition in ramjet engine experiments. We anticipate that the cooperative hydrogen bonding between the polymer and small molecule will pave the way for the development of high-content metallized gel propellants with exceptional stability and superior shear thinning performance.
引用
收藏
页码:356 / 365
页数:10
相关论文
共 41 条
  • [1] [Anonymous], 2014, 50 AIAA ASME SAE ASE, DOI DOI 10.2514/6.2014-3794
  • [2] A functionalized nano-structured cellulosic sorbent aerogel for oil spill cleanup: Synthesis and characterization
    Bidgoli, Hosein
    Mortazavi, Yadollah
    Khodadadi, Abbas Ali
    [J]. JOURNAL OF HAZARDOUS MATERIALS, 2019, 366 : 229 - 239
  • [3] Synthesis and Characterization of Gelled High-Density Fuels with Low-Molecular Mass Gellant
    Cao, Jinwen
    Zhang, Yong-Chao
    Pan, Lun
    Shi, Chengxiang
    Zhang, Xiangwen
    Zou, Ji-Jun
    [J]. PROPELLANTS EXPLOSIVES PYROTECHNICS, 2020, 45 (07) : 1018 - 1025
  • [4] Study on viscosity and surface tension properties of biodiesel-diesel blends and their effects on spray parameters for CI engines
    Das, Mithun
    Sarkar, Mouktik
    Datta, Amitava
    Santra, Apurba Kumar
    [J]. FUEL, 2018, 220 : 769 - 779
  • [5] Dipolar interactions and hydrogen bonding in supramolecular aggregates: understanding cooperative phenomena for 1st hyperpolarizability
    Datta, Ayan
    Pati, Swapan K.
    [J]. CHEMICAL SOCIETY REVIEWS, 2006, 35 (12) : 1305 - 1323
  • [6] Composite oleogels formed by cellulose particles and sorbitan acid esters
    Gao, Zhiming
    Zhang, Chao
    Wu, Yuehan
    Chen, Fangfang
    Hu, Bing
    Wang, Ran
    Yang, Jixin
    Nishinari, Katsuyoshi
    [J]. FOOD STRUCTURE-NETHERLANDS, 2022, 31
  • [7] Ignition and combustion behavior of gel fuel particles with metal and non-metal additives
    Glushkov, D. O.
    Paushkina, K. K.
    Pleshko, A. O.
    Yanovsky, V. A.
    [J]. ACTA ASTRONAUTICA, 2023, 202 : 637 - 652
  • [8] Influence of gellant and drag-reducing agent on the ignition characteristics of typical liquid hydrocarbon fuels
    Glushkov, D. O.
    Kuznetsov, G., V
    Nigay, A. G.
    Yanovsky, V. A.
    [J]. ACTA ASTRONAUTICA, 2020, 177 (177) : 66 - 79
  • [9] Laser ignition of nanocomposite thermites
    Granier, JJ
    Pantoya, ML
    [J]. COMBUSTION AND FLAME, 2004, 138 (04) : 373 - 383
  • [10] Preparation, characterization, and thermal decomposition kinetics of high test peroxide gel
    He, Zhi-cheng
    Yang, Jin-bo
    Nie, Zhan-bin
    Zhou, Xing
    Wu, Jian-jun
    [J]. ACTA ASTRONAUTICA, 2023, 211 : 510 - 517