FUTURE ASTROPHYSICS MISSIONS REQUIRE EFFICIENT, LOW-TEMPERATURE CRYOCOOLERS TO COOL ADVANCED INSTRUMENTS OR…

Public award description

FUTURE ASTROPHYSICS MISSIONS REQUIRE EFFICIENT, LOW-TEMPERATURE CRYOCOOLERS TO COOL ADVANCED INSTRUMENTS OR SERVE AS THE UPPER STAGE COOLER FOR SUB-KELVIN REFRIGERATORS. POTENTIAL ASTROPHYSICS MISSIONS INCLUDE LYNX, THE ORIGIN SPACE TELESCOPE, AND THE SUPERCONDUCTING GRAVITY GRADIOMETER. COOLING LOADS FOR THESE MISSIONS ARE UP TO 300 MW AT TEMPERATURES OF 4 TO 10 K, WITH ADDITIONAL LOADS AT HIGHER TEMPERATURES FOR OTHER SUBSYSTEMS. DUE TO LOW JITTER REQUIREMENTS, A CRYOCOOLER WITH VERY LOW VIBRATION IS NEEDED FOR MANY MISSIONS. IN ADDITION, A MULTI-STAGE COOLER, CAPABLE OF PROVIDING REFRIGERATION AT MORE THAN ONE TEMPERATURE SIMULTANEOUSLY, CAN PROVIDE THE GREATEST SYSTEM EFFICIENCY WITH THE LOWEST MASS. TURBO-BRAYTON CRYOCOOLERS HAVE SPACE HERITAGE AND ARE IDEAL FOR THESE MISSIONS DUE TO NEGLIGIBLE VIBRATION EMITTANCE AND HIGH EFFICIENCY AT LOW TEMPERATURES. THE PRIMARY LIMITATION IN IMPLEMENTING BRAYTON CRYOCOOLERS AT TEMPERATURES BELOW 10 K HAS BEEN THE DEVELOPMENT OF HIGH EFFICIENCY TURBINES. ON THE PROPOSED PROGRAM, CREARE PLANS TO LEVERAGE RECENT DEVELOPMENTS IN GAS BEARING TECHNOLOGY AND LOW-TEMPERATURE ALTERNATORS TO REALIZE A HIGH-EFFICIENCY, LOW-TEMPERATURE TURBINE. ON THE PHASE I PROJECT, WE WILL PERFORM A PROOF-OF-CONCEPT DEMONSTRATION OF THE TURBINE TECHNOLOGY AT TEMPERATURES DOWN TO 4 K. ON THE PHASE II PROJECT, WE WILL BUILD AND DEMONSTRATE AN ADVANCED LOW-TEMPERATURE TURBINE AT TEMPERATURES OF 4 TO 10 K.