Greg,
In response to your query re horsepower and life the following are extracts from the 1995 SAE paper by W. Flower (Lord Corporation) who developed this type of mount.
]Rubber Hysteresis Friction (RHF) DAMPING
An enlarged view of the interface between the elastomeric substrate and the slider indenter is shown in figure 19. The slider indents and travels along the elastomeric layer. Ahead of the slider, a small "bow wave" is built up; and behind the slider, a "trough" exists which gradually recovers from the slider indentation. The magnitude of the bow wave and trough depend on the indentation, velocity of sliding and various elastomer properties. A non-symmetrical, non-uniform pressure field is build up about the slider/elastomer contact patch area opposing slider motion. This results in a motion retarding force composed of frictional and hysteretic
components. This is the force which provides the damping in the RHF damped mount system.
The situation is more complex for the case of multiple, closely spaced sliders, since the recovery properties of the elastomer become critical. If elastomer recovery is too slow, following sliders do not indent the elastomer to the degree that the initial slider does, and the damping from friction is lessened. However, if elastomer recovery is too rapid, the bulk hysteresis loss in the elastomer is reduced and the damping effect from hysteresis is reduced. Both friction and hysteresis damping effects are important.

TEMPERATURE SENSITIVITY OF RHF DAMPING
The temperature sensitivity of elastomer damping is well known]. Tests were conducted on a RHF damper to determine the stiffening influence of low temperatures. Figure 20 shows the ratio of loop area at -40°C to loop area at 20°C obtained at a common input amplitude and frequency. For the first cycle of excitation, at the beginning of the test sequence, the loop area at -40°C is almost three times the loop area measured at room temperature. After accumulating 100 cycles, the loop area ratio drops to about 2.7, the cycling is then discontinued until the next test time. Following one hour from time 0, the loop area ratio for the first cycle is about 2.8, and 2.5 for the 100th cycle. These ratios are approximately constant with accumulated time. Figure 21 shows the same loop area ratio information, but obtained at -20°C relative to 20°C. This data does not include the heating effect of continued cycling and the resultant reduction in loop area ratio.

FATIGUE OF RFH DAMPER MOUNT
Single axis fatigue tests were conducted using the dynamic load and test frequency versus cycles spectrum shown in figure 22 which is typical of the vertical loads seen on a medium duty truck engine mount. The dynamic loads were superimposed on a static load of 408 kgm to simulate engine weight per mount. Figure 23 indicates how the room temperature loop area is retained as fatigue cycles are accumulated. The retention of loop area with cycle accumulation suggests consistent dynamic performance is feasible.

For the RHF damped mount the hysteresis loop curve in figure 13 shows a nonlinear curve suggestive of a mount with supplemental snubbing. Actually the non-linear effect is due to the onset of RHF damping. Up to about ±1.0 mm, the damping function is disconnected or decoupled from the simple rubber mount. The loop area is only 0.09 kN-mm/cycle, but at inputs above ± 1.0 mm, damping from RHF components is added to damping from the simple rubber mount. This is shown more clearly in figure 14 which was taken at ±5.0 mm and 1 Hz. The shaded area indicates the contribution of the RHF damper. The loop area becomes 10.12 kN-mm/cycle.


SUMMARY
RHF damped mounts are shown to provide damping performance somewhat different than similarly sized fluid mounts. They are primarily amplitude sensitive and not strongly frequency sensitive. They will not provide a minimum stiffness at certain frequencies and amplitudes; but neither do they develop significant stiffness increase at high frequency and low amplitudes. Both types of mounts offer amplitude decoupling for enhanced low amplitude isolation.
I hope this is of help.