IMFD Orbit Insert Program
You MUST use IMFD 4.2.1 for this program to work properly!!!! This program does not require much explanation. It is used to make an orbit insertion from hyperbolic approach orbit to a low orbit around the reference planet. You can define the eccentricity or the apoapis distance of the target orbit. The burn integration technique is used for the burn position calculations. This Program might not run 100% efficiently or accurately. The Autoburn might cut off early; if it does, you can switch to Burn Vector View to finish the burn manually.