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 |