The choice of a profile with higher camber allows a landing at a lower speed,
that becomes 'mandatory' at high loads.
Apply here even more 'the observations already made on the flaps.
You may notice a gain in efficiency compared to Standard version arriving at 25.73, an increase in the minimum vertical speed
up to 0.91m/s, a speed of flight required about 28 m/s, and a good deal more energy due to 'increased
load will delight for lovers of acrobatic missile still in slope.