Determination of Rocket Exhaust Gas Temperatures and Emissivities by Infrared Spectral Methods

Format:

Conference/Event

Author/Creator:

Penzias, Gunter J., author.

Conference Name:

National Aeronautic Meeting

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1962

Summary:

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

Notes:

Vendor supplied data

Publisher Number:

620419

Access Restriction:

Restricted for use by site license