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High Energy Liquid Propellants for Rockets

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Advances in Cryogenic Engineering

Part of the book series: Advances in Cryogenic Engineering ((ACRE,volume 4))

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  • 2 Citations

Abstract

High energy rocket propellants (such as fluorine, hydrogen, hydrazine, etc.) are of great interest because they result in large increases in vehicle performance over that possible with conventional propellants. This means that for any mission to be accomplished the size and weight of the vehicle required would be smaller for the high energy propellants than for conventional propellants.

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© 1960 Springer Science+Business Media New York

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Kinney, G.R. (1960). High Energy Liquid Propellants for Rockets. In: Timmerhaus, K.D. (eds) Advances in Cryogenic Engineering. Advances in Cryogenic Engineering, vol 4. Springer, Boston, MA. https://doi.org/10.1007/978-1-4757-0540-9_1

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  • DOI: https://doi.org/10.1007/978-1-4757-0540-9_1

  • Publisher Name: Springer, Boston, MA

  • Print ISBN: 978-1-4757-0542-3

  • Online ISBN: 978-1-4757-0540-9

  • eBook Packages: Springer Book Archive

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