Below you can find comparative data on flight characteristics as calculated in LockOn. This data was taken from official open sources.
Dependence of rate of turn in relation to velocity. A steady turn at an altitude of 200 m above sea level for F-15C aircraft. Data from technical resources and those calculated in LockOn are compared.
This diagram illustrates the F-15C acceleration characteristics in regards to Mach over time at an altitude of 3,050 m with maximum engine thrust. Here you can find the data from official sources and those calculated in LockOn program. You can see just how close they are.
Permissible Flight Data area is an envelope showing permissible values of Altitude/Mach number variables for the F-15C.. Here you can find the data from official sources and those calculated in LockOn.
Comparison of acceleration characteristics for the F-15C and Su-27.
