A Subsonic Analog of the F-111A Airplane,

Abstract

An engineering examination is made of a subsonic analog of the F-111A to determine what savings can be made in terms of weight and cost. It is concluded that so long as both planes have the same mission, both planes will have nearly the same gross takeoff weight. Savings in cost appear to be substantial, however, and a detailed cost analysis is being prepared for sepetate distribution. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 13, 1964
Accession Number
AD0761188

Entities

People

  • R. D. Linnell

Organizations

  • Center for Naval Analyses

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Cost Analysis
  • Costs
  • Engineering

Fields of Study

  • Physics

Readers

  • Aviation Science / Aeronautics.
  • Energy Conservation and Renewable Energy Engineering.
  • Materials Science