Large-scale liquid hydrogen tank rapid chill and fill testing for the advanced shuttle upper stage concept
By: R.H. Flachbart [and six others]
Contributors: George C. Marshall Space Flight Center
Series: NASA/TP -- 2013-217482; NASA technical paper -- 217482
Publisher: National Aeronautics and Space Administration, Marshall Space Flight Center
Published: 2013
Place of publication: Huntsville, Alabama
Language: eng
Number of pages: 43
Subjects: Upper stage rocket engines; Cryogenic fluids; Fluid management; Liquid hydrogen; Film boiling; Heat transfer; Cryogenic cooling; Propellant tanks; Fuel tank pressurization
Notes: Title from title screen (viewed on July 5, 2013).

"April 2013."

Includes bibliographical references (page 43).

Sponsored by National Aeronautics and Space Administration M-1358