Accession Number:

AD0375581

Title:

EVALUATION OF THE COMBUSTION OF A LIGHT METAL HYDRIDE GELLED FUEL WITH SELECTED OXIDIZERS.

Descriptive Note:

Quarterly rept. 1 Apr-30 Jun 66,

Corporate Author:

AEROJET-GENERAL CORP AZUSA CALIF

Personal Author(s):

• Rosenberg,S. D.
• Shoemaker,G. E.

Report Date:

1966-07-01

Pagination or Media Count:

36.0

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

Descriptors:

• (*FUELS
• COMBUSTION)
• OXIDIZERS
• TEST FACILITIES
• TEMPERATURE
• METALS
• SLURRY FUELS
• HYDRIDES (U) (*LIQUID ROCKET PROPELLANTS)
• (*THIXOTROPIC ROCKET PROPELLANTS)
• (*COMBUSTION CHAMBERS)
• BERYLLIUM COMPOUNDS
• METHYL HYDRAZINES
• FLUORINE COMPOUNDS
• METHANE
• VAPOR PRESSURE
• EXHAUST GASES
• TRANSITION METALS

Subject Categories:

• Liquid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE