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.
Determination of Rocket Exhaust Gas Temperatures and Emissivities by Infrared Spectral Methods
Sae Technical Papers
Pre-1964 SAE Technical Papers ; 1906
01.01.1962
Aufsatz (Konferenz)
Englisch
Determination of rocket exhaust gas temperatures and emissivities by infrared spectral methods
Engineering Index Backfile | 1962
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