SITE MAP
 
 

ASTM F-15 Alloy Properties

Chemical Composition %
Nickel 29 Nominal
Cobalt 17 Nominal
Manganese 0.05 Maximum
Silicon 0.20 Maximum
Carbon 0.06 Maximum
Iron Balance Maximum




Thermal Expansion Coefficient

30-4000C (86-7520F) 4.60 to 5.20 x 10-6cm/cm/0C 2.6 to 2.9 x 10-6in/in/0F
30-4500C (86-8420F) 5.10 to 5.50 x 10-6cm/cm/0C 2.8 to 3.1 x 10-6in/in/0F




Physical Properties

Density 8.35 gm/cc 0.302 lb/cu.in.
Melting Point 14500C 26420
Thermal Conductivity
    at 300C (860F) 0.0395 gm cal./sq.cm/sec/0C/cm 0.0318 BTU/sq.ft./0F/in.
    at 3000C (6320F) 0.0485 gm cal./sq.cm/sec/0C/cm 0.0391 BTU/sq.ft./0F/in.

Electrical Resistivity

    at 200C (680F) 49 microhm/sq.cm/cm 294 ohm/cir.mil./ft.
Core Temperature 4350C 8150F




Mechanical Properties

Tensile Strength 52.7 kg/sq.mm 75,000 psi
Yield Strength 0.2% offset 28.1 kg/sq.mm 40,000 psi
Elongation % in 2 in. (5.08cm) 30
Reduction of Area (%) 70
Modulus of Elasticity 14.1 x 103kg/sq.mm 20 x 106 psi
Hardness (Rockwell 15T) 81
Poisson's Ratio 0.30




Linear Thermal Expansion
of F-15 Alloy and Hard Glass
vs. Temperature

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