Knowing the final angle, and the thread pitch, and length of bolt not-in-the-thread, it's straightforward to calculate the %age strain in the bolt, and so the tensile stress it ends up at. Plus there will be some initial tensile stress, which if we assume frictionless tightening, is proportional to the torque applied. (I'm assuming they did it like the wheel nuts, torque to 111 ft-lbs, slacken 45 degrees, tighten to 185 ft-lbs). We can probably knock off 10% to allow for friction reducing effective torque as a reasonable estimate. Question is, does the combined stress exceed yield stress for whatever material is in the stretch bolts? Presumably it must, otherwise you could re-use the existing bolts ad nauseam. The problem then is to determine what stress that actually is, as exceeding this by too large an amount using high-tensile bolts risks stripping the thread in the receiving hole! Do you know what material that hole is tapped into? If it's mild steel, we can calculate the max tensile force it can take as being Pi * bolt_Nominal_Diameter * bolt_Depth_In_Hole * Yield_Shear_Stress_Mild_Steel (half the Yield Tensile Stress will do) and then factor-in whatever safety factor you want.
So hopefully the tensile force required to strip the threaded hole in shear mode greatly exceeds the tensile force in the stretch-bolts at their tensile yield stress! If there's a spare, unused threaded hole in the rear axle (or you're prepared to sacrifice the original one!) you could see what torque is required to strip these holes, using an HT cap-screw.
Young's modulus will be the same for whatever variety of steel is used in these, stretch/high-tensile/mild.
If you're happy with say high-tensile socket-head cap screws as a replacement (I would!) then it should be possible to get some shoulder washers of reasonably hardened steel to suit. If you can't find any of these, I can make you some on my lathe.