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Carbon Deposition Model for Oxygen-Hydrocarbon Combustion, Volume 2Presented are details of the design, fabrication, and testing of subscale hardware used in the evaluation of carbon deposition characteristics of liquid oxygen and three hydrocarbon fuels for both main chamber and preburner/gas generator operating conditions. In main chamber conditions, the deposition of carbon on the combustion chamber wall was investigated at mixture ratios of 2.0 to 4.0 and at chamber pressures of 1000 to 1500 psia. No carbon deposition on chamber walls was detected at these main chamber mixture ratios. In preburner/gas generator operating conditions, the deposition of carbon on the turbine simulator tubes was evaluated at mixture ratios of 0.20 to 0.60 and at chamber pressures of 720 to 1650 psia. The results of the tests showed carbon deposition rate to be a strong function of mixture ratio and a weak function of chamber pressure. Further analyses evaluated the operational concequences of carbon deposition on preburner/gas generator performance. This is Volume 2 of the report, which contains data plots of all the test programs.
Document ID
19880017871
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hernandez, R.
(Aerojet TechSystems Co. Sacramento, CA, United States)
Ito, J. I.
(Aerojet TechSystems Co. Sacramento, CA, United States)
Niiya, K. Y.
(Aerojet TechSystems Co. Sacramento, CA, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1987
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
NAS 1.26:179376
RPT/AA0631/087-VOL-2
REPT-2427-IFR-VOL-2
NASA-CR-179376
Report Number: NAS 1.26:179376
Report Number: RPT/AA0631/087-VOL-2
Report Number: REPT-2427-IFR-VOL-2
Report Number: NASA-CR-179376
Accession Number
88N27255
Funding Number(s)
CONTRACT_GRANT: NAS8-34715
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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