Turbinestarter is a very important composing part for aero-engine, its work capability directly affects the reliability of aero-engine in start.
涡轮起动机是航空发动机的重要组成部分,其工作性能直接影响发动机的起动可靠性。
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In order to validate auxiliary airstart performance of a gas turbinestarter designed only for the ground engine, the test of auxiliary airstart was conducted on the flight test rig.