Description
Precision:
| Ratio of specific heats | γ | |
| Ideal gas constant (J kg-1 K-1) | R |
| Total pressure (Pa) | p0 | |
| Total temperature (K) | T0 | |
| Throat area (m2) | Athroat | |
| Exit area (m2) | Aexit | |
| Critical pressure for sonic throat (Pa) | pcrit | |
| Back pressure for shock at exit (Pa) | pshock-exit | |
| Design back pressure (Pa) | pdesign | |
| Design exit Mach number | Madesign | |
| Maximum mass flow rate (kg s-1) | mdotmax | |