Improved solid performance is needed to meet Integrated High Payoff Rocket Propulsion Technology (IHPRPT) Program goals. The principal objective of this program is to synthesize new hydroxy-terminated oligomers for use in polyurethane binders. These novel oligomers will contain gem-dinitro groups to provide performance advantages compared to currently used propellant components. The materials are expected to have good low-temperature and high-temperature properties, and to be compatible with nitroplasticizers.
Keywords: Chemical Synthesis, Rocket Propellants, Nitro Groups