SOLID-CORE NUCLEAR THERMAL PROPULSION (NTP) HAS BEEN IDENTIFIED AS THE ADVANCED PROPULSION CONCEPT WHICH CO…

Public award description

SOLID-CORE NUCLEAR THERMAL PROPULSION (NTP) HAS BEEN IDENTIFIED AS THE ADVANCED PROPULSION CONCEPT WHICH COULD PROVIDE THE FASTEST TRIP TIMES WITH FEWER SPACE LAUNCH SYSTEM (SLS) LAUNCHES FOR HUMAN MISSIONS TO MARS. CURRENT ENVIRONMENTAL REGULATIONS REQUIRE THAT RADIOACTIVE HALOGENS, NOBLE GASES, AEROSOLS AND PARTICULATES MUST BE FILTERED OUT OF NTP ENGINE EXHAUST DURING GROUND TESTING. IN PHASE I, WE DEMONSTRATED THE ABILITY OF OUR SORBENT TO REMOVE PPM LEVELS OF HALOGENS AND NOBLE GASES FROM HELIUM AT HIGH SPACE VELOCITIES OVER MULTIPLE REGENERATION CYCLES. IN THIS SBIR PHASE II PROJECT, TDA RESEARCH, INC. PROPOSES TO DEVELOP A NOVEL SCRUBBER THAT CONTAINS OUR HIGH-CAPACITY SORBENT TO REMOVE OF THE RADIOACTIVE HALOGENS AND NOBLE GASES FROM NTP ENGINE EXHAUST, AS PART OF NASA'S LARGER EXHAUST TREATMENT SYSTEM. IN PHASE II, WE WILL CONTINUE TO OPTIMIZE THE SORBENT FORMULATION, SCALE UP ITS PRODUCTION, AND DESIGN AND BUILD A PORTABLE SUB-SCALE UNIT TO DEMONSTRATE ITS ABILITY TO SELECTIVELY REMOVE>99.5% RADIOACTIVE HALOGENS AND NOBLE GASES UNDER SIMULATED NTP ENGINE EXHAUST CONDITIONS. BASED ON THE PERFORMANCE RESULTS, WE WILL CARRY OUT A DETAILED DESIGN OF THE FULL-SIZE SCRUBBING SYSTEM FOR TREATING NTP ENGINE EXHAUST AND ESTIMATE ITS SIZE, COST AND ENERGY REQUIREMENTS.