Comment Module Interlinks Aren't Designed for This.... (Score 1) 387
This is most likely impossible because the ISS structure was never designed to take the kind of thrust this would require; massive reinforcement of the module connections would be required at the very least. Even if ion engines could be used in a low-impulse manner (assuming they are built, configured, etc.) to escape LEO, the deceleration burn for lunar orbit insertion would be more abrupt and jarring.