Data are tabulated for two conceptual engines designed for small transport aircraft. These are the 1790 W (2400 shp) class engine and the 3579 kW (4800 shp) class engine for the 0.5 M sub N and 0.7 M sub N airplanes, respectively. All data points required to perform the STAT missions are provided including take-off, climb, cruise, loiter, and fuel allowances. The weight, dimensions, price, and maintenance costs are given as well as the installation criteria and equations used for adjusting horsepower for gearbox loss, and converting horsepower to thrust. Scaling equations are included.
Propulsion Study for Small Transport Aircraft Technology (STAT), Appendix B
1980
11 pages
Report
No indication
English
Small Transport Aircraft Technology (STAT) Propulsion Study
SAE Technical Papers | 1980
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