Interface used to access the Ramjet propulsion options for a missile.
![]() | Gets or sets the efficiency of the burner. |
![]() | Gets or sets the pressure ratio from the burner exit to the entrance. |
![]() | Gets or sets the altitude design point of the engine. |
![]() | Gets or sets the mach number design point of the engine. |
![]() | Gets or sets the thrust design point of the engine. |
![]() | Gets or sets the maximum temperature that the engine material can support. |
![]() | Gets or sets the heating value of the fuel. |
![]() | Gets or sets the pressure ratio from the inlet exit to the entrance. |
![]() | Opt to have no thrust if the fuel is empty. |
![]() | Gets or sets the pressure ratio from the nozzle exit to the entrance. |
![]() | Gets or sets the pressure ratio from ambient conditions to the engine exit. |