Solid Propellant Environmental Effects Digital Twin Modeling Services

The buyer seeks solid propellant environmental effects digital twin services to model and simulate the combined effects of thermal, temporal, chemical, and geometric changes that occur over time in rocket motor grains. The selected vendor must integrate predictive behavior tools into solid rocket motor design tools following Modular Open Systems Approach standards, develop a digital engineering plan, transition non-continuum mechanisms to continuum-based techniques, and anchor predictive models to historical propellant aging data using SysML 2.0 platforms. Eligibility is restricted to onshore United States organizations only, with a projected Level 2 self-assessed CMMC requirement. Vendors will perform work offsite and may submit proposals digitally by email or online.