Advanced HfC-TaC Oxidation Resistant Composite Rocket Thruster |
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Authors: | M C L Patterson S He L L Fehrenbacher J Hanigofsky B D Reed |
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Affiliation: |
a Technology Assessment and Transfer, Annapolis, MD
b Texas Instruments SC Bldg MS37, Dallas, Texas
c NASA Lewis Research Center, Cleveland, OH |
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Abstract: | Several compositions of HfC-TaC codeposited by chemical vapor deposition were evaluated for oxidation protection of graphite substrates. Oxyacetylene torch ablation tests with an O2, C2, H2, ratio of 4:1 were used to test the adherence and composition of the coating and resulting oxides, which were subsequently characterized by x-ray diffraction and scanning electron microscopy. The preferred HfC-TaC composition of 70:30 was used to fabricate a 25 lbf graphite fiber reinforced rocket thruster with a unique structural design. Thruster testing at NASA Lewis was performed at 0.520 MPa chamber pressure and 1650°C (3000°F) using a 6 to 7:1,02,:H2 fuel mixture; a uniform, adherent oxide layer was observed on the internal surface of the combustion chamber following the test. |
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