Combustion Characteristics of a Solid Propellant With a Charring Binder

D E Udlock; L D Strand

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NASA NTRS · 19740032320

Combustion Characteristics of a Solid Propellant With a Charring Binder

D E Udlock·L D Strand

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Abstract

A brief investigation of the combustion characteristics of a solid propellant containing a binder which chars, as opposed to melting or volatizing, has been made. The burning rate of the propellant with the charring binder was significantly higher than similar propellants containing non-charring binders. High speed motion pictures of the burning propellant showed that the aluminum burned on the regressing surface, rather than a short distance from it as is typical with composite propellants.

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BibTeX RIS

D E Udlock, L D Strand. 1973-01-01. Combustion Characteristics of a Solid Propellant With a Charring Binder. https://ntrs.nasa.gov/citations/19740032320

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