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Test Data Analysis of the Thermodynamic Vent System-Augmented Top Spray Injector Liquid Nitrogen Transfer ExperimentsTraditionally, a cryogenic tank must be pre-chilled to some “target” temperature before the main vent valve can be closed to attempt a non-vented fill (NVF) of cryogenic liquid propellant. This methodology is particularly attractive for performing in-space transfer of cryogens due to the unknown location of the liquid/vapor interface in microgravity and the high likelihood of venting liquid if the vent valve is opened during transfer. This paper presents in-depth test data analysis of a Thermodynamic Vent System (TVS) augmented injector used for cryogenic tank chilldown and fill experiments of a thin-walled Titanium tank. Eight tests were conducted using liquid nitrogen across a range of inlet conditions and boundary conditions, and three different chilldown/fill methods. For four of the tests, the injector sprays liquid into the tank as normal, but also uses a TVS heat exchanger to cool the metallic injector itself as well as the main incoming liquid stream. Results show that using the TVS augmented injector simplifies transfer operation via enhanced condensation at the injector surface at the cost of sacrificing only a small amount of propellant.
Document ID
20210024691
Acquisition Source
Glenn Research Center
Document Type
Accepted Manuscript (Version with final changes)
Authors
Jason Hartwig ORCID
(Glenn Research Center Cleveland, Ohio, United States)
Noah Rhys
(Yetispace Huntsville, Alabama, United States)
Jonathan Stephens
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Justin Clark
(The Ohio State University Columbus, Ohio, United States)
Andre LeClair ORCID
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Alok Majumdar ORCID
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Date Acquired
November 20, 2021
Publication Date
May 16, 2022
Publication Information
Publication: International Journal of Heat and Mass Transfer
Publisher: Elsevier
Volume: 194
Issue Publication Date: September 15, 2022
ISSN: 0017-9310
Subject Category
Spacecraft Propulsion and Power
Funding Number(s)
CONTRACT_GRANT: 80GRC019D0001
CONTRACT_GRANT: 80MSFC18C0011
WBS: 012873.05.02.01.22
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Thermodynamic Vent System
Injector
Liquid Nitrogen
No-vent Fill
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