An energetic solid rocket motor propellant having one or more plateau regions of low operating pressure exponent is disclosed. The propellant is formulated from ingredients including an energetic polyoxetane, an effective amount of a plasticizer, an inorganic oxidizer in at least two discrete particle...http://www.google.es/patents/US6217682?utm_source=gb-gplus-sharePatente US6217682 - Energetic oxetane propellants
