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NASA Cryocooler Technology Developments and Goals to Achieve Zero Boil-Off and to Liquefy Cryogenic Propellants for Space ExplorationNASAs interest in human exploration of Mars has driven it to invest in 20K cryocooler technology to achieve zero boil-off of liquid hydrogen and 90K cryocooler technology to achieve zero boil-off liquid oxygen or liquid methane as well as to liquefy oxygen or methane that is produced on the surface of Mars. These investments have demonstrated efficiency progress, mass reductions, and integration insights. A history of the application of cryocooler technology to zero boil-off propellant storage is presented. A trade space on distributed cooling is shown, along with the progress of reverse turbo-Brayton cycle cryocoolers, where the specific power and specific mass have dropped, decreasing the mass and power of these cryocoolers. Additionally, the cryocooler technology advancements of recuperators and compressors are described. Finally, NASAs development ideas with respect to zero boil-off technology are discussed.
Document ID
20180004710
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Plachta, D.
(NASA Glenn Research Center Cleveland, OH, United States)
Stephens, J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Johnson, W.
(NASA Glenn Research Center Cleveland, OH, United States)
Zagarola, Mark
(Creare, LLC Hanover, NH, United States)
Desseranno, David
(Creare, LLC Hanover, NH, United States)
Date Acquired
August 28, 2018
Publication Date
July 7, 2017
Subject Category
Propellants And Fuels
Report/Patent Number
GRC-E-DAA-TN44227
Meeting Information
Meeting: Space Cryogenics Workshop
Location: Chicago, IL
Country: United States
Start Date: July 5, 2017
End Date: July 7, 2017
Sponsors: Cryogenic Society of America, Inc.
Funding Number(s)
WBS: WBS 946870.04.03.04.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
reverse turbo-Brayton cycle cryocooler
zero boil-off
cryogenic propellant storage
Multi-layer insulation
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