A RELIABLE THERMAL MANAGEMENT SYSTEM THAT WILL ENABLE AT LEAST 24-HOURS SURVIVAL OF VENUS LANDERS IN THE EX…

Public award description

A RELIABLE THERMAL MANAGEMENT SYSTEM THAT WILL ENABLE AT LEAST 24-HOURS SURVIVAL OF VENUS LANDERS IN THE EXTREME ENVIRONMENT (460 C, 92 BAR) IS HIGHLY DESIRABLE FOR NASA FUTURE VENUS IN-SITU EXPLORATION MISSIONS. IN RESPONSE TO THE NASA SBIR SOLICITATION, ADVANCED COOLING TECHNOLOGIES, INC. (ACT) PROPOSES TO DEVELOP A CONSUMABLE-BASED COOLING SYSTEM FOR VENUS LANDERS WASTE HEAT REJECTION. THE PROPOSED SYSTEM CONSISTS OF TWO PRESSURIZED VESSELS: A PRIMARY VESSEL CHARGED WITH A CONSUMABLE FLUID IN A SATURATION STATE (AMMONIA) AND A SECONDARY VESSEL FILLED WITH COMPRESSED GAS. THE MAIN ROLE OF THE COMPRESSED GAS IS TO HELP AMMONIA VAPOR VENTING INTO A HIGHER-PRESSURE ENVIRONMENT THAN THE VAPOR PRESSURE THAT CORRESPONDS TO THE COOLED ELECTRONICS TEMPERATURE. THROUGH VENTING A MIXTURE OF CONSUMABLE VAPOR AND COMPRESSED GAS TO THE VENUS AMBIENT, A SIGNIFICANT AMOUNT OF EVAPORATIVE COOLING (PRIMARY) AND JOULE-THOMPSON COOLING (SECONDARY) CAN BE ACHIEVED, WHICH NOT ONLY WILL KEEP THE ELECTRONICS TEMPERATURE COOL BUT ALSO PROVIDE HEAT GUARDING BY COLLECTING AND REMOVING THE INCOMING HEAT LEAKS FROM VENUS ENVIRONMENT. IN PHASE I, A PROOF-OF-CONCEPT CONSUMABLE BASED PROTOTYPE WILL BE FABRICATED AND TESTED. TEST RESULTS WILL BE USED TO VALIDATE A MATHEMATICAL MODEL. AFTER VALIDATION, THE MODEL WILL BE EMPLOYED TO DESIGN THE FULL-SCALE PROTOTYPE AND OPTIMIZE MASS AND THERMAL PERFORMANCE. A PRELIMINARY MODELING RESULT SHOWS A THERMAL MANAGEMENT SYSTEM TOTAL MASS (FLUIDS AND STRUCTURE) OF 75KG.