Perhaps seeing them less as a "VLS" and more as a "augmented flare dispenser" might be more instructive.
I think the size of each "missile" in the "VLS" needs to be properly scaled for us -- for example, this is the goal for the US MSDM, scaled compared to the AMRAAM and Sidewinder, it's very, very small:
And this is a 1:1 scale mockup of the Lockheed MHTK missile (a SAM, but which is very close to the MSDM in concept and considered to be a likely way in which MSDM may be oriented) -- with a missile diameter of only
4 centimeters:
Such missiles (assuming a 4-5cm diameter, let's say needing to reside in a 6x6cm missile cell), packed into the 6x4 grid pack with single offset U shaped VLS vent as depicted in the patent, would see the overall VLS+vent "module" be under 1.2m long and 0.4m wide -- and if you don't include the vent and only consider the VLS missile cells, it would be no longer than 0.6m long.
For a fighter aircraft, that kind of footprint is probably too much.
But for a modern clean sheet bomber design? It is very much realistic.