AI Summary
This RFP seeks novel hypergolic propellants with reduced volatility and toxicity for missile defense systems. The goal is developing safer, cost-effective fuel alternatives that maintain rapid ignition performance while minimizing hazardous vapor emissions compared to traditional formulations.
This topic seeks novel hypergolic fuels featuring significantly reduced volatility and toxicity compared to traditional hypergolic fuels while maintaining rapid, reliable ignition characteristics essential for missile defense applications. Current DACS systems typically use highly toxic and volatile fuels which, while offering excellent ignition delays and specific impulse, present significant handling and safety concerns. The program desires to explore cost-effective alternative fuels that offer reduced vapor pressures while simultaneously minimizing ignition delays to ensure adequate DACS responsiveness in missile defense scenarios. Candidate solutions might include, but are not limited to: ionic liquids, reaction-driven amines, boranes, and others. Hypergolic fuel blends are also an acceptable alternative so long as they could be justified in terms of miscibility and maintained performance across operational temperature ranges.
Objective
Develop and demonstrate low-volatility, reduced-toxicity hypergolic fuels suitable for Divert and Attitude Control System (DACS) thrusters while maintaining critical performance metrics when paired with standard oxidizers.
DSIP Phase Details Available
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