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Author

Title Large-scale liquid hydrogen tank rapid chill and fill testing for the advanced shuttle upper stage concept [electronic resource] / R.H. Flachbart [and six others].

Publication Info.

Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, 2013.

Connect to
Connect to https://permanent.fdlp.gov/gpo37982/20130013526_2013013309.pdf
Connect to https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20130013526.pdf

Location	Call No.	OPAC Message	Status
Axe Federal Documents Online	NAS 1.60:2013-217482	---	Available

Description	1 online resource (vii, 43 pages) : illustrations (some color).
	text txt rdacontent
	computer c rdamedia
	online resource cr rdacarrier
Series	NASA/TP ; 2013-217482
	NASA technical paper ; 217482.
Note	Title from title screen (viewed on July 5, 2013).
	"April 2013."
Bibliography	Includes bibliographical references (page 43).
Funding	Sponsored by National Aeronautics and Space Administration M-1358
Subject	Upper stage rocket engines.
	Cryogenic fluids.
	Fluid management.
	Liquid hydrogen.
	Film boiling.
	Heat transfer.
	Cryogenic cooling.
	Propellant tanks.
	Fuel tank pressurization.
Added Author	George C. Marshall Space Flight Center, issuing body.
Gpo Item No.	0830-H-15 (online)
Sudoc No.	NAS 1.60:2013-217482