Eight mouse eyes (four from 3-month-old and four from 6-month-old animals) were obtained from terminally anesthetized young adult male C57BL/6 mice. Immediately after enucleation, the eyes were cannulated with a 26-gauge needle at 90° to the visual axis with the aid of an operating microscope. Cyanoacrylate glue was used around the point of entry of the needle in the anterior chamber to prevent leakage of aqueous humor. The absence of such leaks was verified microscopically throughout the experiment. IOP was controlled by adjusting the height of a variable column of balanced salt solution (BSS) attached to the cannula (open-stopcock method). IOP was verified and continuously recorded by a pressure transducer (Model TNF-R; Ohmeda, Louisville, CO) connected to the cannula, which was calibrated before eye cannulation by varying the height of the BSS column.
IOP was sequentially adjusted to 5-, 10-, 15-, 20-, 25-, 30-, 35-, 40-, 50-, and 60-cm water pressures (10 mm Hg = 13.6 cm water pressure). The eyes were suspended from the cannulating needle and rested against a vertical backing plate before the cornea being brought into contact with the tonometer probe from a horizontal direction. The tonometer probe and coil assembly were also positioned in a fixed horizontal position by an instrument clamp, so that the probe touched the cornea at its apex. Five measurements were made at each pressure level and the mean was calculated. The starting distance of the probe from the corneal surface was approximately 2.4 mm. Only measurements that occurred within a narrow time window (5 ms) 12 ms subsequent to triggering the tonometer probe were accepted for analysis. The ratio of probe speed immediately before impact over the deceleration during impact with the cornea was related to manometric (true) IOP. Therefore the ratio used for measurement, although given in units of time (seconds), was not derived from direct measurements of the time and distance of probe movement. Instead, the absolute voltage value at the time of impact and the slope of the voltage change after impact were the actual parameters used to determine this ratio. Both of these parameters are directly related to speed and deceleration, respectively, and yield a ratio that is proportional to the ratio of actual speed and deceleration of the probe.