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Volumn PV 2004-16, Issue , 2004, Pages 253-267
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Thermodynamics-based materials selection for corrosion-resistant performance in high-temperature missile propulsion systems. part I. consideration of condensed phase equilibria
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Author keywords
[No Author keywords available]
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Indexed keywords
PROPULSION COMPONENTS;
THERMAL STRESS SENSITIVITY;
ULTRA-HIGH-TEMPERATURE MATERIALS;
CORROSION RESISTANCE;
HAFNIUM;
HIGH PRESSURE EFFECTS;
NOZZLES;
PROPULSION;
REFRACTORY METALS;
THERMAL STRESS;
THERMODYNAMICS;
VAPOR PRESSURE;
CERAMIC MATERIALS;
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EID: 31744445217
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper |
Times cited : (4)
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References (20)
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