"Liquid Rocket Propellant Compatibility Testing."
Item
Dublin Core
Identifier
Liqurockprop.pdf DIVIDED INTO TWO FILES
spc_stnv_000407
Title
"Liquid Rocket Propellant Compatibility Testing."
Description
Material-propellant compatibility as related to liquid rocket propulsion system design criteria is discussed and applicable test methods to derive usable design data are presented. Test methods, with emphasis on metallic materials, are discussed and the shortcomings of a number of these test methods are pointed out. These tests include static immersion tests, stress-corrosion tests, flow tests, impact tests, and tests to determine the effect of cracks and notches in metals on compatibility. A general outline for the evaluation of metallic and nonmetallic materials with respect to propellant compatibility is presented.
Creator
Date
1967-06-28
Temporal Coverage
Source
Saturn V Collection
Box 23, Folder 13
University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
Language
Rights
This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections.
Relation
spc_stnv_000400_000424
Is Referenced By
<a href="http://libarchstor.uah.edu:8081/repositories/2/archival_objects/17703"> View this item in ArchivesSpace. </a>
Collection
Citation
McFarlen, William T., “"Liquid Rocket Propellant Compatibility Testing.",” UAH Archives, Special Collections, and Digital Initiatives, accessed December 26, 2024, http://libarchstor2.uah.edu/digitalcollections/items/show/10881.