Improved rocket nozzle liners for LOX/methane engine designs to replace existing high thermal conductivity materials such as Narloy Z with 50% increased thermal conductivity , lighter weight at similar cost . This approach can be used for any liquid rocket engines including heavy lift. Improved heat exchanger design for environment control for manned spaceflight
Thermal management of electronic devices such as improved heat sinks and spreaders for motor drives CPUs, power electronics and photonics to replace existing Cu/Mo/Cu and copper tungsten composites,
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