X-22A TRI-SERVICE V/STOL AIRCRAFT

Abstract

Designs and release of drawings to manufacturing for fabrication of parts is progressing. Weight Control effort has been maintained, and changes in the target weight are fluctuating with the release of detail design and due to many adjustments resulting from subcontracted systems and changes authorized by Cockpit Mockup Inspection. All changes resulting from Cockpit Mockup Inspection are presently being packaged for formal submittal to BuWeps. Reduction of wind tunnel data from the 1/5 scale, 1/7 scale, and ground effects models progressed. Test preparations for continued wind tunnel model tests were made. The Acoustic Noise Test of the fuselage test specimen as well as the Salt Spray tests and Low cycle-high stress fatigue tests of maraging steel specimens were all completed.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1963
Accession Number
AD0442858

Entities

People

  • A. J. Marchese

Organizations

  • Bell Aircraft Corporation

Tags

Communities of Interest

  • Air Platforms
  • Human Systems
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Airframes
  • Cockpits
  • Control Systems
  • Fuselages
  • Landing Gear
  • Manufacturing
  • Model Basins
  • Navy
  • Radar Altimeters
  • Ship Model Basins
  • Short Takeoff Aircraft
  • Simulators
  • Test And Evaluation
  • Test Facilities
  • Wind Tunnels

Readers

  • Aerospace Engineering
  • Fluid Dynamics.
  • Software Engineering