Accession Number:

AD0442728

Title:

X-22A TRI-SERVICE V/STOL AIRCRAFT

Descriptive Note:

Monthly progress rept. no. 7, 1-30 June 1963

Corporate Author:

BELL AEROSYSTEMS CO BUFFALO NY

Personal Author(s):

Report Date:

1963-07-15

Pagination or Media Count:

55.0

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.

Subject Categories:

  • VSTOL

Distribution Statement:

APPROVED FOR PUBLIC RELEASE