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Limb radiance inversion radiometerEngineering and scientific objectives of the LRIR experiment are described along with system requirements, subassemblies, and experiment operation. The mechanical, electrical, and thermal interfaces between the LRIR experiment and the Nimbus F spacecraft are defined. The protoflight model qualification and acceptance test program is summarized. Test data is presented in tables to give an overall view of each test parameter and possible trends of the performance of the LRIR experiment. Conclusions and recommendations are included.
Document ID
19750013527
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Drozewski, R. W. (Honeywell, Inc. Lexington, MA, United States)
Gille, J. C. (Honeywell, Inc. Lexington, MA, United States)
Thomas, J. R. (Honeywell, Inc. Lexington, MA, United States)
Twohig, K. J. (Honeywell, Inc. Lexington, MA, United States)
Boyle, R. R. (Honeywell, Inc. Lexington, MA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-143712
Report Number: NASA-CR-143712
Accession Number
75N21599
Funding Number(s)
CONTRACT_GRANT: NAS5-21652
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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