Interface used to access the missile options in the Aviator catalog.
![]() | Get the catalog item interface for this object. |
![]() | Set the missile's climb airspeed and airspeed type. |
![]() | Set the missile's max cruise airspeed and airspeed type. |
![]() | Set the missile's descent airspeed and airspeed type. |
![]() | Get the aerodynamics interface. |
![]() | Get the attitude transitions interface. |
![]() | The standard airspeed of the missile while climbing. |
![]() | The climb airspeed type. |
![]() | Opt whether to fail while climbing if there is insufficient specific excess power. |
![]() | The maximum flight path angle of the missile's flight path while climbing. |
![]() | The minimum flight path angle of the missile's flight path while climbing. |
![]() | The missile's default cruising altitude. |
![]() | The maximum airspeed of the missile while cruising. |
![]() | The cruise airspeed type. |
![]() | The aircraft's default configuration as saved in the catalog. |
![]() | The standard airspeed of the missile while descending. |
![]() | The descent airspeed type. |
![]() | Opt whether to fail while descending if there is insufficient specific excess power. |
![]() | The maximum flight path angle of the missile's flight path while descending. |
![]() | The minimum flight path angle of the missile's flight path while descending. |
![]() | The maximum allowable Equivalent Airspeed. |
![]() | Opt whether to ignore the flight path angle limits for climb and descent transitions. |
![]() | The maximum allowable mach number. |
![]() | The mode that the missile will adhere to the specified load factor. Scale by atmospheric density will cause the missile to consider dynamic pressure when calculating turn radius. |
![]() | Get the interface for the Aero/Prop Maneuver Mode helper. The maneuver mode must be set to Aero/Prop to access this interface. |
![]() | The maximum load factor that the missile can withstand while maneuvering. |
![]() | Get the propulsion interface. |
![]() | The maximum total temperature limit of the missile. |
![]() | Opt whether to limit the speed of the missile so the specified Equivalent Airspeed is not exceeded. |
![]() | Opt whether to limit the speed of the missile so the specified mach number is not exceeded. |
![]() | Opt whether to limit the speed of the missile so the specified temperature is not exceeded. |
Implemented Interface |
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IAgAvtrVehicle |
IAgAvtrCatalogItem |
Name |
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AgAvtrMissile |