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Volumn , Issue , 2005, Pages
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The effect of nanosized aluminum on composite propellant properties
a
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Author keywords
[No Author keywords available]
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Indexed keywords
ALUMINUM CONTENTS;
ALUMINUM POWDERS;
BURNING RATE;
COMPOSITE PROPELLANT;
CONCENTRATION OF;
GAP TESTS;
HIGH COSTS;
HIGH-CONTENT;
LOW PURITY;
MAXIMUM STRESS;
METAL FUEL;
MICRON SIZE;
MODULUS OF ELASTICITY;
NANO-SIZED;
NANO-SIZED POWDER;
SECOND GROUP;
STATIC FIRING;
STRAIN AT BREAK;
ULTRAFINE ALUMINUM POWDERS;
AGGLOMERATION;
ALUMINA;
ALUMINUM;
ALUMINUM POWDER METALLURGY;
CHEMICAL ANALYSIS;
COMBUSTION;
CURING;
DURABILITY;
EXPLOSIVES;
MECHANICAL PROPERTIES;
METALLIC GLASS;
PARTICLE SIZE;
POWDER METALS;
PROPELLANTS;
SPACECRAFT PROPULSION;
STRESSES;
THERMOCHEMISTRY;
VISCOMETERS;
VISCOSITY;
IRON OXIDES;
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EID: 77957839812
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper |
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Times cited : (31)
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References (8)
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