A new generation of rocket propellants for deep space exploration, ionic liquid propellants, with long endurance and high stability, is attracting more and more attention. However, a major defect of ionic liquid propellants that restricts their application is the inadequate hypergolic reactivity between the fuel and the oxidant, and this defect results in local burnout and accidental explosions during the launch process. We propose a visualization model to show the features of structure, density, thermal stability, and hypergolic activity for estimating propellant performances and their application abilities. This propellant materials genome and visualization model greatly improves the efficiency and quality of developing high-performance propellants, which benefits the discovery of new advanced functional molecules in the field of energetic materials.

具有长寿命和高稳定性的新一代用于太空探索的火箭推进剂，离子液体推进剂正受到越来越多的关注。然而，限制离子液体推进剂应用的主要缺陷是燃料与氧化剂之间的过高高反应性不足，这种缺陷导致在发射过程中局部烧毁和意外爆炸。我们提出了一个可视化模型，以显示结构，密度，热稳定性和超高活性的特征，以估算推进剂性能及其应用能力。这种推进剂材料的基因组和可视化模型极大地提高了开发高性能推进剂的效率和质量，