Tactical Missile Launcher Feasibility Study. Book II.

Abstract

The document contains inertial load tables and air load tables relative to 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 from 500 to 3,000 pounds, from the F100, F101, F104 and F105 aircraft.

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1968
Accession Number
AD0854199

Entities

Organizations

  • Honeywell International, Inc.

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Feasibility Studies
  • Launchers
  • Launching

Readers

  • Missile Defense Systems.
  • Systems Analysis and Design