VAPOR DEPOSITION OF TUNGSTEN ON ROCKET NOZZLE INSERTS

Abstract

A second beryllia nozzle insert was coated with tungsten. The deposited metal was rough and lacked uniformity. This condition was owing, in part, to difficulty in controlling a slow flow rate of heavy-density tungsten hexachloride vapor. The tungsten-coated beryllia substrate had a transverse crack. Beryllia exposed to reactant gases showed some corrosion.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1961
Accession Number
AD0259441

Entities

People

  • F. W. Hoertel

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Air Force
  • California
  • Corporations
  • Flow Rate
  • Gas Turbine Nozzles
  • Government Procurement
  • Jet Propulsion
  • Materials
  • Military Research
  • Navy
  • New Jersey
  • Nozzles
  • Ordnance Laboratories
  • Rocket Nozzles
  • Rockets
  • United States

Readers

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