X-22A TRI-SERVICE V/STOL AIRCRAFT

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 1/5 scale powered model and are continuing with modified controls. The second series of tests on the 1/6 scale unpowered model were started. TESTING OF Wing Compression Test Panels has been started.

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Document Details

Document Type
Technical Report
Publication Date
Jul 15, 1963
Accession Number
AD0442728

Entities

Organizations

  • Bell Aircraft Corporation

Tags

Communities of Interest

  • Air Platforms
  • Human Systems
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Airframes
  • Airplanes
  • Cockpits
  • Contractors
  • Contracts
  • Control Systems
  • Engineering
  • Fuselages
  • Ground Effect
  • Landing Gear
  • Manufacturing
  • Research Aircraft
  • Short Takeoff Aircraft
  • Test And Evaluation
  • Wind Tunnels

Readers

  • Aerospace Engineering
  • Clinical Trial Research.