Oxygen System Compatibility Test - CF 188 NACES Configuration

Abstract

A series of 84 unmanned tests of the NACES configuration CF188 oxygen system were conducted to demonstrate compatibility of system components reflected by acceptable flow and pressure characteristics. Results confirmed acceptable system performance in each regulator mode and over the operating ranges of inlet pressure, altitude and breathing profile, varied both individually and in combination.

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Document Details

Document Type
Technical Report
Publication Date
Apr 28, 2008
Accession Number
ADA485483

Entities

People

  • R. D. Michas

Organizations

  • Defence Research and Development Canada

Tags

Communities of Interest

  • Autonomy

DTIC Thesaurus Topics

  • Abstracts
  • Air Supplies
  • Aircrafts
  • Altitude
  • Classification
  • Ejection Seats
  • Engineering
  • Flow
  • Ground Level
  • High Altitude
  • Low Altitude
  • Mass Flow
  • Oxygen Masks
  • Regulators
  • Respiration
  • Seats
  • Security

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Electrical Engineering
  • Materials Science

Technology Areas

  • Autonomy