I don't see why not, and I agree with your aesthetic criticism. The Shuttle solid rocket motors had thrust vectoring for attitude control during launch, which is why they had those fat skirts around the base (
compare and
contrast). In a two-motor application, one can imagine that either motor might not have full-azimuth authority. Rather (for example) the right-side motor might not have a nozzle that could vector towards the left side of the vehicle, and so you could mount the motors closer together.
However, (1) this design was derived specifically from the 8.4m system and so I did not have the freedom to relocate the hold-down devices on the base of the solid motors, and (2) aerodynamically it would be suboptimal but totally okay.