Determination of Rocket Exhaust Gas Temperatures and Emissivities by Infrared Spectral Methods
620419
01/01/1962
- Event
- Content
- 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.
- Pages
- 5
- 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.