Comp XFI Lobes
LSK lobe 2126- 273 (.006) - 223 (.050) - 149 (.200) - .636" lift
On profiles and base circles, note that the LS1 has the largest journal except for race blocks. This is writeup is from Crane Cams:
Our roller profiles are designed for a particular finished lobe size, as determined by engine types or base circle radius requirements. We have provided a column indicating the Lobe Design Size for each of the listed profiles. Coding is as follows:
A. 1.786” nominal journal diameter (Buick V-6 and V-8, or special small base circle diameter. Chevrolet 262-400 V-8 requiring connecting rod to cam clearance in long stroke applications.)
B. 1.868” nominal journal diameter (Chevrolet 262-400 and 348-409 V-8 and Pontiac 265-455 V-8)
C. 1.948” to 1.968” or 50 mm journal diameter (Chevrolet 262-400 V-8 LRB, Chevrolet 396-454 V-8, Plymouth-Dodge 273-360, 350-440, & Hemi V-8’s)
D. 2.036” nominal journal diameter (Ford 221-302 and 351C-400 V-8’s), AMC
E. 2.125” nominal journal diameter (Ford 429-460 and other engines)
F. 55 mm or 2.165” nominal journal diameter (Chevrolet LS1 V-8, Chevrolet Vortec V-8, Ford LRB, and other engines)
G. 60 mm or 2.362” nominal journal diameter (Large cubic inch race only engines)
Some lobe designs have had masters generated for more than one size category. These have been indicated where applicable. When a roller lobe designed for one journal size is applied to an engine having a different nominal journal size, a duration change will occur. For example, an “A” lobe ground on a “C” engine camshaft will realize a four-degree increase at 0.050” cam lift. There is usually a two-degree change between design size series. Caution must be used when selecting a larger sized lobe for a smaller lobe application. If a “D” lobe were used on an “A” application, not only would a duration loss of eight degrees take place, but also a negative radius of curvature (inverted flank) may try to occur in the grinding process, resulting in a finished lobe shape that is not representative of the actual design shape. This may result in unstable valve train, possibly causing component failure. Lobes that are intended to have this inverted flank (Crane’s IR series) were carefully designed and manufactured using a special process to prevent this condition. Even so, IR camshafts are not normally advised for high RPM applications.
Last edited by DavidNJ; Feb 10, 2006 at 08:11 AM.
And yes, they do have these lobes on the ls1 core. Comp can do almost any lobe on the ls1 core cause it's so damn big compared to everything.
I believe comp may also be the only company in which lobes don't grow by going from one master size to another (ex. from sbc journal to 55mm ls1 journal). Crane (as indicated above) and cam motion do grow. LSM, i'm not sure about.
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"The 918s don't go into coil bind until 1.085, so take 1.800 (installed height) and subtract 1.085 and you get .715 lift before coil bind. Now subtract another .050 from .715 to account for the distance you should have safely before coil bind and you get .665. That's .665 lift you can safely run with these springs but it's not quite that easy as most cams with that kind of lift have crazy agressive ramps and the 918s will not have enough pressure to control them, unless you use titanium valves or some other crazy stuff or a crazy crazy slow lobe. Now, let's say you plan to use a cam with .615 lift. You could shim up the comp 918 springs till they are .050 from binding when that lift figure is taken to account. To do this simply take the .665 lift number and subtract .615 lift and you come up with the shim thickness that you need to run this spring at .050 from coil bind with a .615 lift cam. In this particular case you would need .050" worht of shims.
You would do this to increase the pressure of this spring to aid in controlling the agressive ram rate cams. Just an example."
Is really close to the LSK lobe, fast ramp but with less lift or is it closer to the XER lobe?
The XFI questions seem to be piling up.

