Method for measuring suitability of aluminum for use in certain

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73 15R, 73 35, G01R 2702

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039581764

ABSTRACT:
The resistance of aluminum particles which contain aluminum oxide coatings is measured while the particles are being slowly heated. The resistance is plotted against temperature. If the resistance drops off to zero before the temperature reaches 660.degree.C, the particles are undesirable for use as a fuel in certain rocket propellants.

REFERENCES:
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patent: 3701278 (1972-10-01), Askins et al.
patent: 3899919 (1975-08-01), Geisler et al.
Crawford, Jr. et al., Direct Determination of Burning Rates of Propellant wders, Analytical Chemistry, Feb. 1947, pp. 630-633.
Spenadel, Burning Rate Measurement of Solid Propellants, The Review of Scientific Instruments, July 1961, pp. 837-839.

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