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Long-Term Cryogenic Space Storage System

  • R. A. Hopkins
  • W. L. Chronic
Conference paper
Part of the Advances in Cryogenic Engineering book series (ACRE, volume 18)

Abstract

The requirements associated with long-term storage of cryogens for space vehicle applications necessitate continued improvements in insulation and zero-g fluid venting technology. Key considerations in the development of such systems are thermal performance, weight, and reliability. Evacuated multilayer insulation is the only type of insulation which is presently developed and feasible for these applications.

Keywords

Thermal Performance Insulation System Heat Leak Thermal Protection System Lower Temperature Level 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

  1. 1.
    J. E. Bell, “Final Report/Design Manual—Propulsion Cryogenic Tankage for Extended Mission Capabilities,” Beech Aircraft Corporation ER 15961, NASA Contract NAS 9–10348, July 1971.Google Scholar
  2. 2.
    K. E. Leonhard and E. H. Hyde, Cryogenic Technology, 7 (1): 12 (1971).Google Scholar
  3. 3.
    R. T. Parmley, “Microspheres—A New High Performance Cryogenic Insulation,” Lockheed Missiles and Space Company, presented at Marshall Space Flight Center, Cryogenic Workshop, March 29, 1972.Google Scholar
  4. 4.
    G. R. Cunnington, C. W. Keller and G. A. Bell, “Thermal Performance of Multilayer Insulations,” Interim Rept., Lockheed Missiles and Space Company, NASA CR72605, April 1971.Google Scholar

Copyright information

© Springer Science+Business Media New York 1973

Authors and Affiliations

  • R. A. Hopkins
    • 1
  • W. L. Chronic
    • 1
  1. 1.Boulder DivisionBeech Aircraft CorporationBoulderUSA

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