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Accession Number:
AD0375581
Title:
EVALUATION OF THE COMBUSTION OF A LIGHT METAL HYDRIDE GELLED FUEL WITH SELECTED OXIDIZERS.
Corporate Author:
AEROJET-GENERAL CORP AZUSA CALIF
Report Date:
1966-07-01
Abstract:
Design and fabrication of a 1000-lb-thrust test engine facility is nearly complete. The engine will be used for determining combustion and performance efficiencies of the following systems 1 TNMBeH220 MMH80, 2 TNM80 TFH20BeH220 MMH80, and 3 TNM60 TFH40BeH220 MMH80. Provisions for the containment and sampling of the beryllium-containing exhaust solids will be provided. Base-line firing of TNMMMH will precede the candidate system testing. Author
Descriptive Note:
Quarterly rept. 1 Apr-30 Jun 66,
Pages:
0036
Contract Number:
AF 04(611)-11535
File Size:
0.00MB
