Design of Storable Propellant Pressure Vessels

660677

2/1/1966

Authors
Abstract
Content
Four considerations in the design of storable propellant structures are: stress caused by load and pressure requirements, sealing surfaces and bolted tank closures, corrosion and stress corrosion, and material compatibility. This paper discusses the developmental background of these considerations in connection with the Titan family.
Specific items discussed are design and fabrication of the basic tankage, especially sealing problems, and the compatibility of materials with amine fuels and nitrogen tetroxide.
Meta TagsDetails
DOI
https://doi.org/10.4271/660677
Citation
Heymans, R., Thompson, E., and Berman, L., "Design of Storable Propellant Pressure Vessels," National Aeronautic and Space Engineering and Manufacturing Meeting, Los Angeles, California, United States, October 3, 1966, https://doi.org/10.4271/660677.
Additional Details
Publisher
Published
2/1/1966
Product Code
660677
Content Type
Technical Paper
Language
English