Determination of Rocket Exhaust Gas Temperatures and Emissivities by Infrared Spectral Methods 620419
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.
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. Download Citation
Author(s):
Gunter J. Penzias, Stanley A. Dolin, Richard H. Tourin
Pages: 5
Event:
Pre-1964 SAE Technical Papers
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Rocket engines
Radiation
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