Here are some thoughts/experience from my military electronic design and shock mounting (including cases):
Any shock isolation system (rack cases included) MUST have both a compliant suspension system and some form of energy damping to provide a reduction in shock load from the external (the environment) to the internal (the protected element).
In order to do this, manufacturers use a compliant element (think of a car suspension spring) and a damping element (car shock absorber). The goal is to reduce the peak shock (measured in G force... example 1000 G's, dropped from 3 feet on plywood) to a lower G (shock) peak value (example 50 G's, common limit for electronics innards). What happens really is that the sharp external G load is converted into a lower peak G shock but also makes the load duration longer (widens the pulse of shock). To accomodate this conversion, the spring element provides the isolation and the damping (shock absorber) converts some of the energy into heat (yup, that is really what happens).
In order to provide the ability for the spring to move, some distance is required between the internal and external surfaces. This is called 'sway space' and is a key factor in the limitation of the shock protection system. Heavier internal loads (mass, i.e. pounds of stuff) require stiffer springs and sufficient sway space so the compliant 'springs' can allow for shock to be absorbed. Stiffer 'shock absorbers, i.e. dampers will raise the internal shock loading but are needed to keep the protected element from just bouncing around on the 'spring system'.
The bottom line is that the design of ANY shock mounting system must consider: The internal mass of the protected stuff, the worst case external shock loading (G load and shock pulse waveform), the requirement for limitation of protected stuff (G load and damped/stretched shock waveform), the repetitive shocks or single event (i.e. airframe crash loading or vehicle transport vibration). These input parameters to the design of the shock mounting system then yield the need for sway space (3 dimensional, i.e. X/Y/Z axis). Other vibrational loads (like aircraft engine vibration isolation, etc.) are also considered (example is an A-10 Warthog GAU-2 gattling gun vibration into the airframe and all avionics).
Specifically on the OP mentioned case, the front and back foam (said to be 1/2" thick) is really the shock isolation compliance (springs) and damping (the foam converts the motion into heat). Normal isolation 'boxes' use shock mounts at all 8 corners (rectangular systems), this is provided in a distributed manner with this foam. There is no need for 'shock mounts' to be located in locations other than these points (or in this case the front/back interfaces).
I hope this helps in shock mounting understanding.. Yes, I'm an engineer (35 years in DOD electronics design including mechanical, thermal, optical, RF, communications, processing and former USAF lab coat guy)... and now I'm unemployed (yes, I watched 'Falling Down' ironically the day prior to the layoff)... Shock mounting is a science but is easily modeled today with common mechanical CAD programs.
Pete