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Brake control system modification, augmentor Wing Jet STOL Research Airplane (AWJSRA)The braking system for a short takeoff aircraft is discussed and the deficiencies are described. The installation of a Boeing 727 aircraft brake system was made to correct the deficiencies. Tests of the modified system were conducted using an analog computer/hardware simulator. Actual performance tests were conducted and the characteristics of the system were satisfactory.
Document ID
19740021261
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Amberg, R. L. (Boeing Commercial Airplane Co. Renton, WA, United States)
Arline, J. A. (Boeing Commercial Airplane Co. Renton, WA, United States)
Jenny, R. W. (Boeing Commercial Airplane Co. Renton, WA, United States)
Date Acquired
September 3, 2013
Publication Date
June 24, 1974
Subject Category
Aircraft
Report/Patent Number
D6-41896
NASA-CR-137530
Report Number: D6-41896
Report Number: NASA-CR-137530
Accession Number
74N29374
Funding Number(s)
CONTRACT_GRANT: NAS2-7641
PROJECT: RTOP 766-71-01-01-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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