Stress Analysis of Aircraft Modifications (C-141B Aircraft). Joint Airborne Communications Center/Command Post (JACC/CP) Provisions,

Abstract

Stress Analyses were performed on the following aircraft modifications: AT1108 Antenna Installation, HF Longwire Installation, UPS-192 Antenna Installation, 437S-1C Antenna Installation, and SATCOM Antenna Installation. The detailed conclusions of each of the topics above are contained after each sub-analysis. However, the general conclusion is that each of the subject modifications in no way impare the airworthiness of the aircraft in that the aircraft strength is equal to or greater than the original unmodified strength. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Oct 27, 1980
Accession Number
ADA095634

Entities

People

  • D. B. Ragan

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Forces
  • Aerodynamic Loading
  • Aircraft Panels
  • Aircrafts
  • Aluminum Alloys
  • Attachment
  • Civil Engineering
  • Elements
  • Engineering
  • Joints
  • Level Flight
  • Plastic Explosives
  • Sea Level
  • Stress Analysis
  • Stresses
  • Structural Components
  • Thickness

Readers

  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Software Engineering
  • Structural Health Monitoring of Composite Structures.

Technology Areas

  • Fully Networked C3
  • Fully Networked C3 - Command and Control