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Particle Impact Simulation and Ignition Prediction

Completed TRL 7 (started at 6, targeting 7)

Description

An experimentally calibrated tool is needed to predict if an oxidizer system is susceptible to failure by particle impact ignition based on use conditions, materials, and flow geometry. This tool will accelerate new components, evaluating existing hardware, and help disposition anomalies.

Benefits

This tool will accelerate design, assessing existing hardware, and disposition of anomalies. Given the number of vehicles in development, now is relevant for WSTF to collaborate with academia, industry, and the NESC to fundamentally understand PI. New testing technology in combination with higher fidelity flowing PI conditions performed at WSTF can anchor models of PI. Computational tools for modeling particle interactions with flow, and high strain rate hydrocode allow for fundamental understanding of ignition behavior.

Details

Technology areaPropulsion Systems > Chemical Space Propulsion > Integrated Systems and Ancillary Technologies
ProgramCenter Innovation Fund: JSC CIF (JSC CIF)
Lead organizationJohnson Space Center, Houston, TX
Start date2023-10-01
End date2024-09-30

Project contacts

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How to get involved

This is a mature technology (TRL 7) — the realistic path in is usually NASA's Technology Transfer Program: licensing an existing NASA patent, or a Space Act Agreement to use NASA facilities/expertise directly. NASA also runs a startup licensing program with no upfront fee for companies formed to commercialize a specific NASA technology.

None of these are guaranteed paths for this specific project — TechPort itself doesn't have an "apply" button. Reaching out to the contact(s) above with a specific question is usually the fastest way to find out what's actually open.