Highly Survivable Truss Type Tail Boom,

Abstract

Successful completion of Army helicopter missions in future battle scenarios may well depend upon survival of the structure after battle damage. Survivability of a helicopter will depend significantly upon the structure's ability to retain structural integrity. The principle purpose of this study is to develop a structural concept which assures a high degree of confidence in the integrity of a structure that has received combat damage. This study has been pursued because the Army needs to meet and provide a solution to the ever escalating high explosive anti-aircraft threat to the helicopter tail boom.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1978
Accession Number
ADA056430

Entities

People

  • Thomas F. Erline

Organizations

  • Ballistic Research Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Airframes
  • Aluminum Alloys
  • Army Aircraft
  • Buckling
  • Computer Programs
  • Computers
  • Damage
  • Damage Tolerance
  • Dynamic Loads
  • Explosives
  • Flight Loads
  • Helicopters
  • High Explosives
  • Margin Of Safety
  • Modulus Of Elasticity
  • Safety
  • Structural Integrity

Readers

  • Aviation Science / Aeronautics.
  • Sensor Fusion and Tracking Systems.
  • Strategic Security Studies