Title: Altitude Performance Characteristics of the J73-GE-1A Turbojet Engine
Abstract: From Introduction: over-all altitude-performance characteristics of this engine are reported herein, and the component performance characteristics are given in reference 1. The data are presented in the form of engine pumping characteristics to allow accurate calculation of engine performance at any operating or flight condition within the range covered by the experimental data. A curve is also presented that will allow determination of thrust in flight by the measurement of ambient static pressure and total pressure in the exhaust nozzle.
Publication Year: 1954
Publication Date: 1954-12-09
Language: en
Type: article
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