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Design Factors for Liquid Hydrogen Rocket Engine Test Facilities
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English
Abstract
Thermodynamic properties of liquid hydrogen and their relationship to the design of rocket engine test facilities are presented. Major points covered are the need to completely define the thermodynamic state of the liquid, and a method of determining the heat gain during flow from the environment and from fluid friction. Charts useful for estimating these effects are included.
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Authors
Citation
Folkerts, K. and Hoag, E., "Design Factors for Liquid Hydrogen Rocket Engine Test Facilities," SAE Technical Paper 630373, 1963, https://doi.org/10.4271/630373.Also In
References
- Jacobs, R. B. “Liquid Requirements for the Cool Down of Cryogenic Equipment,” Boulder, Colorado National Bureau of Standards August 1962
- Jacobs, R. B. “Single Phase Transfer of Liquified Gases,” Washington Government Printing Office, National Bureau of Standards Circular 596 1958
- Richards, R. J. Steward, W. C. Jacobs, R. F. “Transfer of Liquid Hydrogen through Uninsulated Line,” Boulder, Colorado National Bureau of Standards
- Roder, M. M. Goodwin, R. D. “Provisional Thermodynamic Functions for Para-Hydrogen,” Washington U. S. Dept of Commerce, Office of Technical Services, National Bureau of Standards December 1961