MALFUNCTION OF IGNITERS IN THE AMRA VARIABLE PARAMETER ROCKET ENGINE

Abstract

Three firing tests on nozzles were rendered unsatisfactory due to malfunctioning of the pyrotechnic igniters. These igniters were off-the-shelf manufacturer's items. Failure of the igniters was manifested by the leakage of hot gases through the squib end of the igniter body case, followed by complete erosion of that element resulting in a deleterious decrease in chamber pressure and extension of burning time. Although the igniters were several years old, the manufacturer did not believe that aging was the problem. Subsequent examination of the igniters indicated the presence of corrosion of the electrical lead wire immediately adjacent to the ceramic seal enclosing the primer charge. In order to minimize further mishaps, the manufacturer replaced the primer charge unit in all of the igniters remaining on hand.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1965
Accession Number
AD0626273

Entities

People

  • Anthony K. Wong
  • James Brown

Organizations

  • United States Army Research Laboratory

Tags

DTIC Thesaurus Topics

  • Chambers
  • Combustion
  • Combustion Chambers
  • Engineering
  • Engines
  • Hot Gases
  • Ignition
  • Lead Wires
  • Massachusetts
  • Materials
  • Materials Engineering
  • Propellants
  • Rocket Engines
  • Rockets
  • Solid Propellants
  • Static Tests
  • Test And Evaluation

Readers

  • Rocket Propulsion.
  • Software Engineering
  • Surface Engineering/Surface Coating Technology.