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Aluminum to Stainless-Steel Joints for Cryogenic Applications Aluminum to stainless-steel joints are necessary for cryogenic applications such as cryogenic fluid management and combustion devices. Supplemental development in this area was required for a test program at NASA Marshall Space Flight Center (MSFC) of an Al6061-RAM2 additively manufacturing liquid rocket nozzle. The test program identified a risk for installing stainless-steel fluid fittings to aluminum manifolds. To address this, a literature search was completed for various joint designs, and three designs were down selected to be cryogenic pressure cycle tested at MSFC. The test pieces were subsequently burst tested with ambient temperature water. This paper provides an overview of the literature review, down selected designs, test setup, test results, and fractography. The test results informed design decisions for the Al6061-RAM2 nozzle, and the recommended design proved to be a robust option with no notable issues identified during hot-fire testing.
Document ID
20240006712
Acquisition Source
Marshall Space Flight Center
Document Type
Extended Abstract
Authors
Tessa M. Fedotowsky
(Marshall Space Flight Center Redstone Arsenal, United States)
Claire E. Handley
(Marshall Space Flight Center Redstone Arsenal, United States)
Dalton M. Luedke
(Marshall Space Flight Center Redstone Arsenal, United States)
Paul R. Gradl
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
May 23, 2024
Subject Category
Aircraft Design, Testing and Performance
Space Sciences (General)
Meeting Information
Meeting: 2025 AIAA SciTech
Location: Orlando, FL
Country: US
Start Date: January 6, 2025
End Date: January 10, 2025
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
WBS: 585777.08.20.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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