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When using glycidyl azide binders in propellants, the chemist typically face the following challenges: ‒ insufficient mechanical properties, ‒ high glass transition temperature (cured GAP binder ~ ‒35 °C), ‒ filler-binder interactions, ‒ high mixing and casting viscosities during processing, which limits the maximum filler content, ‒ low reactivity during curing due to the secondary hydroxyl如果在配方中存在水的痕迹，可能会导致侧反应的组，并且当使用与一级羟基的链条扩展/交联三一个时，也有问题的固化， - 极性粘合剂中能量填充物的溶解度， - 价格。主要挑战之一是实现推进剂的良好机械性能。火箭推进剂的机械性能由粘合剂网络，填充物和粘合剂/填充物相互作用确定。
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