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Extraterrestrial Cryogenic Propellants Reliquefaction

  • Conference paper
Advances in Cryogenic Engineering

Part of the book series: Advances in Cryogenic Engineering ((ACRE,volume 11))

Abstract

A number of space missions are predicated on long-duration extraterrestrial storage of cryogens. These range from the exploration of the lunar surface by means of wheeled vehicles powered by hydrogen-oxygen fuel cells to rocket-powered interplanetary travel using hydrogen alone (nuclear rocket) or hydrogen and oxygen, fluorine or flox as the propellants. These missions involve storage periods up to in excess of one year. Consequently, the development of lightweight, low-boiloff-rate propellant storage systems is a prerequisite to the successful accomplishment of these missions.

Work sponsored by the NASA George C. Marshall Space Flight Center under Contract No. NAS 8–5298.

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References

  1. J. W. Dorsey, “Earth Lunar Transportation System—Lunar Propellant Storage,” Martin-Marietta Corporation Report ER 12387-I, Contract NAS 8–1531, Task No. 2 (May 1962).

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  2. T. A. Sedgwick et al., “Hydrogen Reliquefiers for Lunar Storage Systems,” The Marquardt Corporation, Report 6033, Contract NAS 8–5298 (March 12, 1964).

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© 1966 Springer Science+Business Media New York

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Sedgwick, T.A., Middleton, R.L. (1966). Extraterrestrial Cryogenic Propellants Reliquefaction. In: Timmerhaus, K.D. (eds) Advances in Cryogenic Engineering. Advances in Cryogenic Engineering, vol 11. Springer, Boston, MA. https://doi.org/10.1007/978-1-4757-0522-5_27

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  • DOI: https://doi.org/10.1007/978-1-4757-0522-5_27

  • Publisher Name: Springer, Boston, MA

  • Print ISBN: 978-1-4757-0524-9

  • Online ISBN: 978-1-4757-0522-5

  • eBook Packages: Springer Book Archive

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