MS3217C
Table V. Limit loads
0S Shaft (Ref) |
Allowable thrust load for ring assemblies with parts having maximum corner radii or chamfers |
||
From |
To |
Carbon steel or CRES |
Beryllium copper |
---- ---- ---- .591 ---- .750 1.062 1.500 1.938 |
.394 .473 .500 .625 .669 1.000 1.378 1.772 2.000 |
450 LB 550 LB 650 LB 750 LB 900 LB 2500 LB 4000 LB 5000 LB 6000 LB |
300 LB 400 LB 450 LB 550 LB 650 LB 1800 LB 2900 LB 3600 LB 4300 LB |
4. Changes from previous issue. Marginal notations are not used in this revision to identify changes with respect to the previous issue due to the extent of the changes.
MILITARY INTEREST
Custodians: Preparing activity: Army - AR DLA - IS
Navy - OS
Air Force - 99 (Project 5325-2011-004)
NOTE: The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online database at https://assist.daps.dla.mil
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