Normal rockets reach max Q at around Mach 1 after one minute of acceleration. That would happen about 10km up where the air pressure is only about 1/3rd of what it is at the surface. From there on, the air density drops faster than the increase of the forces due to going faster.
For normal rockets, this is such a critical event that they accept longer pull of gravity and throttle back to reduce the stresses on the vehicle. (At least Falcon 9 and Space shuttle do this).
So these guys are going to accelerate stuff to 8000m/s at ground level and then throw it up in the air at ground-level-pressure. Air friction is going to be about 3x (pressure) * 25*25 (speed differential squared!) times more of an issue. That's significant.
Oh.... One more thing... If you give something orbital speed at ground level, ignoring air friction, it will go into an orbit with at best the lowest point at the place where you started. In that case you're launching horizontal, meaning you'll encounter about 200km of air instead of the normal 10km of air starting mostly up.
One last back-of-the-envelope calculation. Orbital speed is about 8000m/s. Humans riding to space can handle 3G for a few minutes, but lets assume we're talking satellites, so 10G is acceptable. So 100m/s^2. That means max Omega (rad/sec) is max 80. So your launch facilty will need an 8000m/s / 80/s = 100m radius launch facility. Do you know anybody who can make a 200m diameter vacuum chamber? (that you're going to explosively re-compress at launch?)
Throwing stuff hundreds of feet into the air is not a problem. Throwing stuff into orbit is.