path: root/3685/CH21/EX21.5/Ex21_5.txt

 
 Example 21.5

 Propulsive power = 7.764351 MW,
 Thrust power = 4402.359492 kW,
 Propulsive efficiency = 56.699645 percent
 Thermal efficiency = 31.057404 percent,
 Overall efficiency = 17.609438 percent