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Measurement of Injector Face Temperature Using Optical Diagnostic TechniquesA CCD camera was previously set up to record infrared images of the injector face of a small rocket combustor. Good semi-quantitative results were obtained but it was found that non-linearities in the camera system made accurate determinations of temperature difficult. A Pulnix CCD camera was purchased and calibrated. The system was calibrated for temperatures between 500 and 850 C. The best filter to use was found to be a BG850 glass filter. The actual calibrations are presented in the report. The system was to be used on a hydrogen oxygen system but the tests did not take place as scheduled. Attempts were made with a methane oxygen system but the carbon in the system interfered with the viewing of the injector face.
Document ID
20000036594
Acquisition Source
Marshall Space Flight Center
Document Type
Contractor or Grantee Report
Authors
Moser, Marlow D.
(Alabama Univ. Huntsville, AL United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1999
Subject Category
Optics
Funding Number(s)
CONTRACT_GRANT: NASA Order H-28520-D
CONTRACT_GRANT: NAS8-97095
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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