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Tank Applied Testing of Load-Bearing Multilayer Insulation (LB-MLI)
Author(s) -
Wesley L. Johnson,
David W. Plachta,
Juan G. Valenzuela,
Jeffrey R. Feller
Publication year - 2014
Publication title -
49th aiaa/asme/sae/asee joint propulsion conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2014-3581
Subject(s) - cryocooler , liquid hydrogen , materials science , shield , thermal insulation , shields , nuclear engineering , heat shield , thermal , pipe insulation , heat load , cryogenics , insulation system , hydrogen , mechanical engineering , environmental science , composite material , vacuum insulated panel , engineering , electromagnetic shielding , thermodynamics , chemistry , petrology , physics , organic chemistry , layer (electronics) , geology
The development of long duration orbital cryogenic storage systems will require the reduction of heat loads into the storage tank. In the case of liquid hydrogen, complete elimination of the heat load at 20 K is currently impractical due to the limitations in lift available on flight cryocoolers. In order to reduce the heat load, without having to remove heat at 20 K, the concept of Reduced Boil-Off uses cooled shields within the insulation system at approximately 90 K. The development of Load-Bearing Multilayer Insulation (LB-MLI) allowed the 90 K shield with tubing and cryocooler attachments to be suspended within the MLI and still be structurally stable. Coupon testing both thermally and structurally were performed to verify that the LB-MLI should work at the tank applied level. Then tank applied thermal and structural (acoustic) testing was performed to demonstrate the functionality of the LB-MLI as a structural insulation system. The LB-MLI showed no degradation of thermal performance due to the acoustic testing and showed excellent thermal performance when integrated with a 90 K class cryocooler on a liquid hydrogen tank.

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