A Zero-Gravity Thermodynamic Vent System for the Shuttle/Centaur Hydrogen Tank

840976

07/01/1984

Event
Intersociety Conference on Environmental Systems
Authors Abstract
Content
A thermodynamic vent system (TVS) is being designed and built by Sundstrand for the Shuttle/Centaur LH2 tank based on concepts developed under previous General Dynamics Convair (GDC)/NASA studies and laboratory demonstrations. The TVS performs the function of controlling pressure in the liquid hydrogen tank during periods of low-gravity storage and assures venting of vapor from the cryogenic propellant tank without disturbing normal Shuttle operation. Major components of the TVS are a swirl flow heat exchanger, an electric mixer pump with fully redundant thermally conditioned electronic inverter, and parallel redundant throttling regulators with filters and shutoff valves.
Meta TagsDetails
DOI
https://doi.org/10.4271/840976
Pages
10
Citation
Sorensen, G., Niggemann, R., Bassett, C., and Sedillo, M., "A Zero-Gravity Thermodynamic Vent System for the Shuttle/Centaur Hydrogen Tank," SAE Technical Paper 840976, 1984, https://doi.org/10.4271/840976.
Additional Details
Publisher
Published
Jul 1, 1984
Product Code
840976
Content Type
Technical Paper
Language
English