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There are a total of 5 record(s) matching your query.
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Effect of water on hydrogen permeability
Author(s): Hulligan, David; Tomazic, William A.
Abstract: Doping of hydrogen with CO and CO2 was developed to reduce hydrogen permeation in Stirling engines by forming a low permeability oxide coating on the inner surface of the heater head tubes. Although doping worked well, under ...
NASA Center: Glenn Research Center Publication Year: 1987
Added to NTRS: 2005-10-13
Accession Number: 87N16664; Document ID: 19870007231; Report Number: DOE/NASA-50112-68, E-3321, NAS 1.15:88898, NASA-TM-88898
Effect Of Water On Permeation By Hydrogen
Author(s): Tomazic, William A.; Hulligan, David
Abstract: Water vapor in working fluid equilibrates with permeability-reducing oxides in metal parts. Report describes study of effects of water on permeation of heater-head tubes by hydrogen in Stirling engine. Experiments performed ...
NASA Center: Glenn Research Center Publication Year: 1988
Added to NTRS: 2005-09-30
Accession Number: 88B10583; Document ID: 19880000583; Report Number: LEW-14648
Hot piston ring tests
Author(s): Allen, David J.; Tomazic, William A.
Abstract: As part of the DOE/NASA Automotive Stirling Engine Project, tests were made at NASA Lewis Research Center to determine whether appendix gap losses could be reduced and Stirling engine performance increased by installing an ...
NASA Center: Glenn Research Center Publication Year: 1987
Added to NTRS: 2005-08-25
Accession Number: 88N14486; Document ID: 19880005104; Report Number: DOE/NASA/50112-72, E-3808, NAS 1.15:100256, NASA-TM-100256
Comparison of hydrazine-nitrogen tetroxide and hydrazine-chlorine trifluoride in small-scale rocket chambers
Author(s): Rollbuhler, R. James; Tomazic, William A.
Abstract: No Abstract Available
NASA Center: Glenn Research Center Publication Year: 1959
Added to NTRS: 2005-08-25
Accession Number: 89N70615; Document ID: 19890068242; Report Number: NASA-TN-D-131
Theoretical Performance of Hydrogen-Oxygen Rocket Thrust Chambers
Author(s): Sievers, Gilbert K.; Tomazic, William A.; Kinney, George R.
Abstract: Data are presented for liquid-hydrogen-liquid-oxygen thrust chambers at chamber pressures from 15 to 1200 pounds per square inch absolute, area ratios to approximately 300, and percent fuel from about 8 to 34 for both ...
NASA Center: Glenn Research Center Publication Year: 1961
Added to NTRS: 2005-08-25
Document ID: 19980227353; Report Number: NASA-TR-R-111
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