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Study of Thermodynamic Vent and Screen Baffle Integration for Orbital Storage and Transfer of Liquid HydrogenA comprehensive analytical and experimental program was performed to determine the feasibility of integrating an internal thermodynamic vent system and a full wall-screen liner for the orbital storage and transfer of liquid hydrogen (LH2). Ten screens were selected from a comprehensive screen survey. The experimental study determined the screen bubble point, flow-through pressure loss, and pressure loss along rectangular channels lined with screen on one side, for the 10 screens using LH2 saturated at 34.5 N/cm2 (50 psia). The correlated experimental data were used in an analysis to determine the optimum system characteristics in terms of minimum weight for 6 tanks ranging from 141.6 m3 (5,000 ft3) to 1.416 m3 (50 ft3) for orbital storage times of 30 and 300 days.
Document ID
19730025004
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cady, E. C.
(McDonnell-Douglas Astronautics Co. Huntington Beach, CA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1973
Subject Category
Propellants
Report/Patent Number
NASA-CR-134482
MDC-G4798
Accession Number
73N33737
Funding Number(s)
CONTRACT_GRANT: NAS3-15846
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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