Oxygen System Compatibility Test

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Authors
  1. Michas, R.D.
Corporate Authors
Defence R&D Canada - Toronto, Toronto ONT (CAN)
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.
Keywords
aircraft, oxygen system, test, compatibility
Report Number
DRDC-TORONTO-TN-2008-072 — Technical Note
Date of publication
28 Apr 2008
Number of Pages
92
DSTKIM No
CA031118
CANDIS No
529832
Format(s):
Electronic Document(PDF)

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