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Accession Number:
AD0442728
Title:
X-22A TRI-SERVICE V/STOL AIRCRAFT
Corporate Author:
BELL AEROSYSTEMS CO BUFFALO NY
Report Date:
1963-07-15
Abstract:
Final design resolutions are being made which incorporate revisions required for the improved longitudinal and directional stability. Flight control system design weight has been established. Further weight control studies are continuing. Wind Tunnelmodel tests have been resumed on the 15 scale powered model and are continuing with modified controls. The second series of tests on the 16 scale unpowered model were started. TESTING OF Wing Compression Test Panels has been started.
Descriptive Note:
Monthly progress rept. no. 7, 1-30 June 1963
Pages:
0055
Distribution Statement:
Approved for public release; distribution is unlimited.
Contract Number:
NOW-63-0118CI
File Size:
4.63MB
