Published By National Aeronautics and Space Administration
Issued over 9 years ago
US
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Summary
Description
We propose to develop a miniature, low RF noise ignition module for NOFBX propulsion systems. This ignition module is designed utilizing unique properties of the NOFBX propellant to enable a potential 2-3 order magnitude reduction in spark ignition energy, voltage, current, and power under a very special set of condition realized only in an NOFBX combustion chamber.