T53-L-703 Military Qualification Test Program
Abstract
New engine models require testing to evaluate design concept, to endurance and flight test hardware so as to insure satisfactory mission effectiveness, and to demonstrate adequacy for release to production. The report describes the results of these tests on two modified turboshaft engines.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1975
- Accession Number
- ADA012657