X-22A TRI-SERVICE V/STOL AIRCRAFT

Abstract

Preliminary design work, performance and weight studies, and calculation reviews of various configurations which are in progress will be reduced to the detail systems and component levels. The Wind Tunnel program, design, fabrication, and test is essentially on schedule. Proposals from vendors for the design, fabrication, test, and delivery of the Transmission Systems (gearboxes and shafting) are being reviewed and evaluated. The Escapac ID (BA) seat was selected for use on this aircraft.

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Document Details

Document Type
Technical Report
Publication Date
Apr 15, 1963
Accession Number
AD0442867

Entities

Organizations

  • Bell Aircraft Corporation

Tags

Communities of Interest

  • Air Platforms
  • Human Systems
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Air Force
  • Aircrafts
  • Airframes
  • Cockpits
  • Contracts
  • Control Systems
  • Ejection Seats
  • Fabrication
  • Fuselages
  • Landing Gear
  • Pressure Measurement
  • Short Takeoff Aircraft
  • Test And Evaluation
  • Test Facilities
  • Wind Tunnel Tests
  • Wind Tunnels

Readers

  • Aerospace Engineering
  • Aerospace Test and Evaluation
  • Software Engineering.