Skip to main content

Thermal Analysis and Optimization of Cryogenic Tanks for Lunar Storage

  • Conference paper
Advances in Cryogenic Engineering

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

Abstract

Exploration of the moon will require hydrogen and oxygen to power roving vehicles and for life support. The long-term storage of these cryogens necessitates low-heat-leak tanks whose design presents a critical technical problem. This paper presents the results of analytical work on the thermal analysis and weight optimization of such tanks.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 39.99
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 54.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. J. R. Oliver and W. M. McCombs, “Lunar Storage of Small Quantities of Cryogenic Fluid,” Report No. TR-4–42–2-D, Kennedy Space Center, Future Studies Branch (January 21, 1964).

    Google Scholar 

  2. J. B. Romero, “Propellant Tank Thermal Analysis with Lunar Storage of Cryogens as Examples,” Boeing Document D2–90673–1 (January 28, 1965).

    Google Scholar 

  3. D. B. Mackay, Design of Space Power Plants, Prentice Hall, Inc., Englewood Cliffs, N.J. (1963), p. 2.

    Google Scholar 

  4. J. M. Saari and R. W. Shorthill, “Isotherms of Crater Regions on Illuminated and Eclipsed Moon,” Icarus 2:115 (1963).

    Article  Google Scholar 

  5. E. Kehat, B. A. Buffham, P. M. Silverberg, and R. G. Clark, “Analysis of Cryogenic Feed Systems for Electrothermal Engines,” Air Products and Chemicals, Inc., Summary Report, Project No. 03–1–4290 (October 1961).

    Google Scholar 

  6. J. Fowler, “Boeing Multilayer Insulation for Cryogenic Tank Systems Applicable to Space Missions,” Boeing Document D2–23242 (May 13, 1964).

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 1966 Springer Science+Business Media New York

About this paper

Cite this paper

Romero, J.B., Smith, D.W., Dod, R.E. (1966). Thermal Analysis and Optimization of Cryogenic Tanks for Lunar Storage. 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_26

Download citation

  • DOI: https://doi.org/10.1007/978-1-4757-0522-5_26

  • Publisher Name: Springer, Boston, MA

  • Print ISBN: 978-1-4757-0524-9

  • Online ISBN: 978-1-4757-0522-5

  • eBook Packages: Springer Book Archive

Publish with us

Policies and ethics