“…AP is currently the state-of-the-art oxidizer for solid rocket propellants due to its impressive oxygen content (OB +34.0%), good burning properties, and low cost of manufacture. , However, health concerns related to unburned perchlorates as well as environmental and tactical issues stemming from HCl generation have spurred widespread efforts to replace AP in propellant formulations. − One chlorine-free oxidizing salt that has been considered as a replacement is AN (Figure ). AN is inexpensive to manufacture and has good oxygen content (OB +20.0%) but suffers from handling issues related to hygroscopicity, poor morphology, and, critically, exhibits a solid state phase transition accompanied by a 3% change in volume during exposure to typical operating temperatures. , AN is also a notoriously poor burning material with an endothermic dissociation to nitric acid and ammonia that inhibits self-sustained burning. , Cocrystallization of AN with a variety of small-molecule coformers has recently been accomplished and shown to mitigate the phase transition . Although cocrystallization can address the major deficiencies of AN, maintaining positive oxygen content of the resultant cocrystals is an unmet challenge; no cocrystals of AN, or indeed any nonperchlorate oxidizing salt (for a successful example using sodium perchlorate, see Inoue et al), have yet achieved a positive oxygen balance, making them nonfunctional as oxidizers.…”