IGF::OT::IGF NASA HAS IDENTIFIED NUCLEAR THERMAL PROPULSION (NTP) AS A PROPULSION CONCEPT WHICH COULD PROVI…

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IGF::OT::IGF NASA HAS IDENTIFIED NUCLEAR THERMAL PROPULSION (NTP) AS A PROPULSION CONCEPT WHICH COULD PROVIDE THE FASTEST TRIP TIMES TO MARS AND AS THE PREFERRED CONCEPT FOR HUMAN SPACE TRAVEL. THE CURRENT NASA STRATEGIC SPACE TECHNOLOGY INVESTMENT PLAN STATES NTP IS A HIGH PRIORITY TECHNOLOGY NEEDED FOR FUTURE HUMAN EXPLORATION OF MARS. IN ORDER TO PERFORM COMPONENT TESTING IN SUPPORT OF NTP ENGINE DEVELOPMENT, AN EFFICIENT MEANS FOR DELIVERING HIGH-FLOWRATE, HIGH-TEMPERATURE HYDROGEN IS REQUIRED. NON-NUCLEAR GENERATION OF THE DESIRED HYDROGEN FLOWRATES AND TEMPERATURES FOR GROUND TEST OF NTP COMPONENTS AND SUBSYSTEMS IS PROBLEMATIC. ACENT LABORATORIES IS PROPOSING DEVELOPMENT HYDROGEN WAVE HEATER (HWH) FOR THIS APPLICATION. THE HWH IS AN INNOVATIVE EMBODIMENT OF A WAVE ROTOR. WAVE ROTORS CAN BE USED AS A PRIMARY COMPRESSOR/HEATER OR AS A TOPPING COMPRESSOR/HEATER TO MULTIPLY THE TEMPERATURE AND PRESSURE OF AN EXISTING COMPRESSION OR HEATING PROCESS. THESE HIGHLY-SCALABLE CONTINUOUS-FLOW DEVICES ARE CAPABLE OF FLOW RATES UPWARDS OF 100 LB/S AND TEMPERATURES OVER 5000 F.