INVESTIGATION OF ATLAS F-SERIES FLAME DEFLECTOR PRESSURE PULSE

Abstract

Presented are the results of a test program to determine the effects of the pressure pulse that is generated in the flame deflector during initial thrust buildup of the Atlas MA-3 booster engine.

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Document Details

Document Type
Technical Report
Publication Date
Aug 15, 1963
Accession Number
AD0415401

Tags

Communities of Interest

  • Materials and Manufacturing Processes
  • Weapons Technologies

DTIC Thesaurus Topics

  • Acoustic Measurement
  • Check Valves
  • Deflection
  • Deflectors
  • Engineering
  • Flame Deflectors
  • Fluids
  • Heat Shields
  • Instrumentation
  • Measurement
  • Measuring Instruments
  • Pressure Measurement
  • Propulsion Systems
  • Sodium Compounds
  • Sustainer Engines
  • Test Stands
  • Thrust Chambers

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Missile Defense Systems.
  • Optical Physics and Photonics.