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Determination of Rocket Exhaust Gas Temperatures and Emissivities by Infrared Spectral Methods
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English
Abstract
Rocket engine exhaust gas temperature and spectral emission are important in design and development of rocket engines. A technique of monochromatic radiation pyrometry and instrumentation for applying the technique have been developed. Results of nine rocket engine firings are presented.
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Citation
Penzias, G., Dolin, S., and Tourin, R., "Determination of Rocket Exhaust Gas Temperatures and Emissivities by Infrared Spectral Methods," SAE Technical Paper 620419, 1962, https://doi.org/10.4271/620419.Also In
References
- Tourin R. H. Grossman M. Combustion & Flame 2 1958 330
- Tourin R. H. “Temperature, Its Measurement and Control in Science and Industry,” III Herzfeld C. M. Reinhold New York 1962 46
- Tourin R. H. J. Opt. Soc. Am. 51 1960 175
- Arnold Center Facilities Handbook, Air Research and Development Command, USAF January 1961 2 4