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Properties of 7000 Series Aluminum Alloys at Cryogenic Temperatures

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Advances in Cryogenic Engineering

Part of the book series: Advances in Cryogenic Engineering ((ACRE,volume 6))

Abstract

Very low temperatures are encountered in current and proposed missiles and space vehicles due to title use of cryogenic propellants such as liquid oxygen and liquid hydrogen and due to the near absolute zero temperatures encountered under certain conditions in outer space. Tjerefore, the properties of engineering materials at these extreme subzero temperatures are becoming of prime importance to the design engineer.

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References

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© 1961 Springer Science+Business Media New York

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Christian, J.L., Watson, J.F. (1961). Properties of 7000 Series Aluminum Alloys at Cryogenic Temperatures. In: Timmerhaus, K.D. (eds) Advances in Cryogenic Engineering. Advances in Cryogenic Engineering, vol 6. Springer, Boston, MA. https://doi.org/10.1007/978-1-4757-0534-8_64

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  • DOI: https://doi.org/10.1007/978-1-4757-0534-8_64

  • Publisher Name: Springer, Boston, MA

  • Print ISBN: 978-1-4757-0536-2

  • Online ISBN: 978-1-4757-0534-8

  • eBook Packages: Springer Book Archive

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