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Zero-G thermodynamic vent system for shuttle/CentaurViewgraphs are presented showing drawings of Centaur configurations, the Thermodynamic Vent System (TVS), the mixer pump, and the hydrogen vent motor pump inverter. A cryogenic performance summary is given in chart form. The TVS liquid flow operation and vapor flow operation are diagrammed.
Document ID
19880006561
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Niggemann, Richard E. (Sundstrand Corp. Rockford, IL, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1987
Publication Information
Publication: NASA. Lewis Research Center, Cleveland, Ohio. Cryogenic Fluid Management Technology Workshop. Volume 1: Presentation Material and Discussion
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
88N15943
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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