Redesign of the Particle-Impact Shock Tube and Preliminary Data Analysis

Abstract

The particle-impact shock tube (PST) located at The Aerospace Corporation provides a test environment to investigate the ignition resistance of metals in high-pressure, oxygen-rich conditions. It is important to characterize candidate alloys intended for use in rocket engines for their ignition resistance. The PST has recently undergone rebuilding and modifications, namely with a new expansion region and test section made entirely of hardened Monel K500, and the addition of a copper liner in the test section. This redesign provides improvements to both the safety of the experiment, as well as allowing its operation with higher oxygen fill pressures than previously permitted (fill pressures above 2000 psi are now accessible). This report discusses the circumstances that led to the rebuild, the details of the redesign, and a preliminary look at the performance of the PST with the new expansion region and test section.

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Document Details

Document Type
Technical Report
Publication Date
Jul 29, 2020
Accession Number
AD1120565

Entities

People

  • James H Morehart
  • Joshua D. Winner

Organizations

  • The Aerospace Corporation

Tags

Communities of Interest

  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Data Analysis
  • Ecology
  • Energy
  • Failure Mode And Effect Analysis
  • Frequency
  • Heat Transfer
  • High Pressure
  • Impact Shock
  • Manufacturing
  • Materials
  • Materials Laboratories
  • Metals
  • Models
  • O Rings
  • Pressure Measurement
  • Rocket Engines
  • Shock Tubes
  • Shock Waves
  • Temperature Gradients
  • X Ray Spectroscopy

Fields of Study

  • Physics

Readers

  • Materials Science and Engineering.
  • Mathematics or Statistics
  • Software Engineering

Technology Areas

  • Space
  • Space - Hall-Effect Thruster