Designed supersonic nozzle

Specific heat ratio

1.31

Total pressure

2000 kPa

Total temperature

2500 K

Inlet

Mach number

1.7

Pressure

354.6 kPa

Temperature

1530 K

Diameter of nozzle

30.0 mm

Cross sectional aria

706.9 mm²

Outlet

Mach number

3.7

Pressure

101.3 kPa

Temperature

400 K

Diameter of nozzle

83.8 mm

Cross sectional aria

5515.4 mm²