Actions for Infrared suppressor effect on T63 turboshaft engine performance

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Infrared suppressor effect on T63 turboshaft engine performance

Author
Civinskas, K. C.
Published
Sep 1, 1978.
Physical Description
1 electronic document
Additional Creators
Walker, C. L. and Bailey, E. E.
Online Version

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Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Tests were conducted to determine if there are performance penalties associated with the installation of infrared (IR) suppressors on the T63-A-700 turboshaft engine. The testing was done in a sea-level, static test cell. The same engine (A-E402808 B) was run with the standard OH-58 aircraft exhaust stacks and with the ejector-type IR suppressors in order to make a valid comparison. Repeatability of the test results for the two configurations was verified by rerunning the conditions over a period of days. Test results showed no measurable difference in performance between the standard exhaust stacks and the IR suppressors.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19790002872.
Accession ID: 79N11043.
E-9730.
AVRADCOM-TR-78-38(PL).
NASA-TM-78970.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15727320