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NASA rotor system research aircraft flight-test data report: Helicopter and compound configurationThe flight test activities of the Rotor System Research Aircraft (RSRA), NASA 740, from June 30, 1981 to August 5, 1982 are reported. Tests were conducted in both the helicopter and compound configurations. Compound tests reconfirmed the Sikorsky flight envelope except that main rotor blade bending loads reached endurance at a speed about 10 knots lower than previously. Wing incidence changes were made from 0 to 10 deg.
Document ID
19840024311
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Erickson, R. E.
(NASA Ames Research Center Moffett Field, CA, United States)
Kufeld, R. M.
(NASA Ames Research Center Moffett Field, CA, United States)
Cross, J. L.
(NASA Ames Research Center Moffett Field, CA, United States)
Hodge, R. W.
(Sikorsky Aircraft Co. Stratford, Conn., United States)
Ericson, W. F.
(Sikorsky Aircraft Co. Stratford, Conn., United States)
Carter, R. D. G.
(Sikorsky Aircraft Co. Stratford, Conn., United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1984
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:85843
NASA-TM-85843
Accession Number
84N32381
Funding Number(s)
PROJECT: RTOP 532-03-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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