X750 Alloy
X750 Alloy is an age-hardenable material, used for its good Creep-Rupture strength at elevated temperatures up to 1500F. It also has a high resistance to oxidation & corrosion. X750 Alloy is used in applications that require optimum resistance to relaxation in springs operating at temperatures up to about 1200F
Common specifications used for X750 Alloy are AMS 5699 and AMS 5698.
Chemical requirements AMS 5698F and AMS 5699F
Elements
N
Cr
Fe
Mn
Cb
Ti
Al
Comp. %
70.0 min.
14.0-17.0
5.0-9.0
1.0 max.
.70-1.20
2.25-2.75
.40-1.00
Elements
C
Cu
Si
S
Co
Ta
Comp. %
.08 max.
.50 max.
.50 max.
.010 max.
1.0 max.
.05 max.
Density/lbs/cu in.
Modulus of elasticity,psi
        Tension
        Torsion
Poisson Ratio
.298
 
31,000,000
11,000,000
.29
Tensiles per AMS 5698
As drawn
Min.  Max.
-----  150 ksi
130 ksi 165 ksi
Size
Up to .025, incl.
over .025 to .500 incl.
After Precipitation Heat Treatment
 (1350 F for 16 hours)
Size
Up to .025 incl.
over .025 to .500 incl.
Min. tensiles
155 ksi
165 ksi
Tensiles per AMS 5699
As drawn
Size
Up to .250, incl.
over .250 to .625 incl.
Min. tensiles
190 ksi
160 ksi
After Precipitation Heat Treatment
Short cycle (1200 F for 4 hours)
Size
.012 to .250 incl.
over .250 to .418 incl.
over .418 to .625 incl.
Min. tensiles
220 ksi
200 ksi
180 ksi
After Precipitation Heat Treatment
Long cycle (2100 F for 2 hours + 1550 F for 24 hours +      1300 F for 20 hours)
Size
Up to .250, incl.
over .250 to .625 incl.
Min. tensiles
150 ksi
145 ksi
The information and data presented herein are typical or average values and are not guarantee of maximum or minimum values. Applications specifically suggested for material described herein are made solely for the purpose of illustration to enable the reader to make his own evaluation and are not intended as warranties, either express or implied, of fitness for these or other purposes.
 
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