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Laser angle sensor developmentElectrical and optical parameters were developed for a two axis (pitch/roll) laser angle sensor. The laser source and detector were mounted in the plenum above the model. Two axis optical distortion measurements of flow characteristics in a 0.3 transonic cryogenic tunnel were made with a shearing interferometer. The measurement results provide a basis for estimating the optical parameters of the laser angle sensor. Experimental and analytical information was generated on model windows to cover the reflector. A two axis breadboard was assembled to evaluate different measurement concepts. The measurement results were used to develop a preliminary design of a laser angle sensor. Schematics and expected performance specifications are included.
Document ID
19810018971
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Pond, C. R.
(Boeing Aerospace Co. Seattle, WA, United States)
Texeira, P. D.
(Boeing Aerospace Co. Seattle, WA, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1980
Subject Category
Lasers And Masers
Report/Patent Number
NASA-CR-159385
Report Number: NASA-CR-159385
Accession Number
81N27509
Funding Number(s)
CONTRACT_GRANT: NAS1-15987
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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