| Ambient Input | Description |
| W | gas path flow[pps] |
| Alt | Altitude(ft) |
| dTamb | Delta Temperature from Ambient [degF] |
| MN | Mach Number [frac] |
| Ambient Output | Description |
| GasPthCharOut | Gas Path Characteristics Output, 5x1 vector consisting of:
- W - gas path flow [pps] - ht - enthalpy [BTU/lbm] - Tt - Total Temperature [degR] - Pt - Total Pressure [psia] - FARc - Combusted Fuel to Air Ratio [frac] |
| Pamb | Ambient Static Pressure [psia] |
| A_Data | Ambient additional calculation Data (3x1 vector):
- Ts - Static Temperature [degR] - Ps - Static Pressure [psia] - Veng - Engine Velocity [ft/sec] |
| Ambient Mask Variable | Description |
| X_A_AltVec_M | Ambient Altitude Vector (mx1) |
| T_A_TsVec_M | Ambient Static Temperature Table Vector (Ts = f(Alt)) (mx1) |
| T_A_PsVec_M | Ambient Static Pressure Table Vector (Ps = f(Alt)) (mx1) |
| AFARc_M | Ambient air quality (combusted Fuel to Air Ratio) [frac] |
| X_A_FARVec_M | Fuel to Air Ratio Vector(fx1) |
| T_A_RtArray_M | Gas Constant, R, Array (R = f(FAR))(fx1) |
| Y_A_TVec_M | Temperature Vector(tx1) |
| T_A_gammaArray_M | Gamma Array (Gamma = f(T,FAR))(txf) |