The ICRNE technology addresses the needs of Subtopic H2.02 In-Space Propulsion Systems, which requests "high temperature materials, coatings and/or ablatives or injectors, combustion chambers, nozzles, and nozzle extension." We expect the ICRNE technology to have direct and immediate application for RCS thrusters, OMS engines, upper stage engines, planetary ascent and descent engines, and new booster engines. Beyond the needs of NASA, the DOD also requires advanced nozzle technology for new upper stage engines and boosters. If successful, the ICRNE technology can be used to join dissimilar materials for a very broad range of applications in many industries, including wing leading edges for high speed transport aircraft, airbreathing engines, turbines, industrial burners, and corrosion-resistant structures for naval vessels.
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