Alternative Processing to Electrodeposition to form Thrust Chamber Structural Jackets

Abstract

Identify, demonstrate, and develop a method of forming a liquid rocket engine thrust chamber structural jacket that is less expensive than electrodeposition and capable of applying nanostructured materials. Document and demonstrate cost and/or weight advantages over conventional electrodeposition of nickel.

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Document Details

Document Type
Technical Report
Publication Date
Feb 28, 2002
Accession Number
ADB282731

Entities

People

  • J. S. Shelley

Organizations

  • Air Force Research Laboratory

Tags

DTIC Thesaurus Topics

  • Abstracts
  • Air Force
  • Air Force Research Laboratories
  • Chambers
  • Data Rights
  • Department Of Defense
  • Electrodeposition
  • Export Controls
  • Information Operations
  • Military Research
  • Rocket Engines
  • Sensitivity
  • Standards
  • Thrust Chambers

Readers

  • Combustion and Flow Dynamics.
  • Surface Engineering/Surface Coating Technology.
  • Systems Analysis and Design

Technology Areas

  • Microelectronics