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Testing of TVS Augmented Injectors for Tank-to-Tank Transfer of CryogensNASA is developing reusable cryogenic systems to enable manned missions to the Moon and Mars. These cryogenic systems will require replenishing cryogens on-orbit via a tanker or propellant depot with minimal loss to boil-off. Three additively manufactured injectors augmented with a Thermodynamic Venting System have been developed for use in tank-to-tank cryogenic fluid transfer. A Vented Chill/No-Vent Fill approach to tank-to-tank transfer has been the industry standard and is explored in this work with emphasis on injector spray patterns and compared to the Charge-Hold-Vent chill method.
Document ID
20220017650
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Nicole Vaughn
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Jonathan Stephens
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Kevin Pedersen
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Travis Belcher
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Cameron Hines
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Omar Mireles
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Noah Rhys
(Jacobs (United States) Dallas, Texas, United States)
James W Smith
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Date Acquired
November 22, 2022
Subject Category
Propellants And Fuels
Meeting Information
Meeting: AIAA Scitech 2023
Location: National Harbor, Maryland
Country: US
Start Date: January 23, 2023
End Date: January 27, 2023
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 012873.05.01.03.62
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Cryogenic Transfer
Propellant Storage
Thermodynamic Venting System
Cryogenic Injector
Tank-to-Tank Transfer
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