I assume you're talking about the Hohmann transfer [0], which is the most efficient path a ship could take. We're not optimizing for efficiency here, we're optimizing for delivery. You should also realize that while there is a specific moment of peak efficiency in launch times, you have a window on the order of months before a Hohmann transfer becomes less efficient than other methods. Once every 2 years sounds less drastic when it's 6 months out of those 2 years.
All that being said, the Hohmann transfer is a lot sketchier in practice than one would think. Neither Mars nor Earth has a perfectly circular orbit. It's often easier just to take the old-fashioned route.
Take a look at this chart [1] for an idea of the spread of trip length vs launch time.
[0] http://www.planetary.org/multimedia/space-images/charts/hohm...
[1] https://mars.jpl.nasa.gov/spotlight/images/porkchop_lg.gif