Tactical Missile Launcher Feasibility Study. Book I.

Abstract

The document describes the development and the results of a study of the feasibility of designing a standard tactical missile launcher which is capable of carrying and launching hypothetical stores, weighing form 500 to 3,000 pounds, from the F100, F101, F104, and F105 aircraft. Store trajectories and flight clearances were investigated in a computer program. The results of the computer runs are analyzed and discussed. Structural and mechanical criteria have been established. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1968
Accession Number
AD0854198

Entities

Organizations

  • Honeywell International, Inc.

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Ascent Trajectories
  • Clearances
  • Computer Program Documentation
  • Computer Programs
  • Computers
  • Feasibility Studies
  • Launchers
  • Launching
  • Standards
  • Trajectories

Readers

  • Aerodynamics/Aeronautics.
  • Computational Modeling and Simulation
  • Missile Defense Systems.