Rheological and Thermal Behavior of Gelled Hydrocarbon Fuels

被引:27
|
作者
Arnold, R. [1 ]
Santos, P. H. S. [2 ]
Campanella, O. H. [2 ]
Anderson, W. E.
机构
[1] Purdue Univ, Dept Aeronaut & Astronaut, Maurice J Zucrow Labs, W Lafayette, IN 47907 USA
[2] Purdue Univ, Dept Agr & Biol Engn, W Lafayette, IN 47907 USA
关键词
PROPELLANT ROCKET ENGINES; VAPORIZATION ENTHALPY; COMBUSTION; LIQUID; RP-1; COMPATIBILITY; HISTORY;
D O I
10.2514/1.48936
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Rocket propulsion systems are bound to energetic propellant combinations to provide the best performance in conjunction with smallest possible storage volume. The application of a gelled fuel and a gelled oxidizer potentially combines the advantages of conventional solid and liquid propellants without some specific disadvantages of both individual systems. Gelled JP-8 and RP-1 fuels have been used to study the rheological behavior of gelled hydrocarbons. For all investigations fumed silica was used as a gelling agent with 4 to 7 wt%. Alongside a description of the gel mixing process, the paper discusses viscosity, stability, thixotropic behavior, and the viscoelastic properties of the gels through their storage and loss moduli as a function of gelling-agent amount. An extended Herschel-Bulkley model was applied to describe the viscosity characteristics of the hydrocarbon gels. Differential scanning calorimetry measurements showed only a slight influence of the gelling-agent amount on the heat of vaporization of the gels. The ungelled hydrocarbons featured a higher heat of vaporization than the gels.
引用
收藏
页码:151 / 161
页数:11
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