Precooling technology is a widely used method for increasing the flight speed of aero-engine by installing a precooler in front of compressor. However, the traditional precooler is difficult to meet the precooling requirement in a wide range because of the fixed geometric structure. In this paper, a novel precooling strategy based on multi-module is proposed, in which the precooler is divided into multiple identical modules and the number of modules cooled by different fuels could be regulated, so as to meet the precooling requirement under different working conditions. To evaluate the performances of this scheme, a one-dimensional model of precooler is established. Besides, the characteristics of heat transfer and decomposition of ammonia are experimentally studied to support the precooler design. The study shows that the heat sink of ammonia reaches 4.59 MJ/kg at 629 °C, and the fitted heat transfer correlation equation matches well with the experimental values within the error of 15 %. Further, in the range of Ma2.5 – 2.88, the precooling demand can be satisfied by using only RP-3, and above Ma2.88, it is necessary to use both NH3 and RP-3 simultaneously. Moreover, the optimal number of precooler module division is 5, and the modular precooling scheme could improve the specific impulse by 24.06 % at Ma3.4 compared to non-modular precooling scheme.
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