Product Description
A nickel-chromium-iron-molybdenum alloy with outstanding strength and oxidation resistance at temperatures to 2200°F (1200°C). Matrix stiffening provided by the molybdenum content results in high strength in a solid-solution alloy having good fabrication characteristics. Used in gas turbines, industrial furnaces, heat-treating equipment and nuclear engineering.
STANDARD PRODUCT FORMS
Sheet, strip, plate, round bar, flat bar, forging stock,
hexagon, wire and extruded section.
hexagon, wire and extruded section.
MAJOR SPECIFICATIONS
UNS N06002
ASTM B 366, B 435, B 572,
B 619, B 622, B 626,
B 751, B 775, B 829
ASME SB-366, SB-435, SB-572,
SB-619, SB-622, SB-626,
SB-751, SB-775, SB-829
DIN 17744, 17750-17754
SAE AMS 5536, 5587, 5588,
5754, 5798
Werkstoff Nr. 2.4665
NACE MR-0175/ISO 15156
AECMA Pr EN 2182 – 2185
BS HR 6, HR 204
ISO 6207, 6208, 9723 – 9725
ASTM B 366, B 435, B 572,
B 619, B 622, B 626,
B 751, B 775, B 829
ASME SB-366, SB-435, SB-572,
SB-619, SB-622, SB-626,
SB-751, SB-775, SB-829
DIN 17744, 17750-17754
SAE AMS 5536, 5587, 5588,
5754, 5798
Werkstoff Nr. 2.4665
NACE MR-0175/ISO 15156
AECMA Pr EN 2182 – 2185
BS HR 6, HR 204
ISO 6207, 6208, 9723 – 9725
LIMITING CHEMICAL COMPOSITION, %
Ni........Remainder
Cr......20.5 – 23.0
Fe...... 17.0 – 20.0
Mo....... 8.0 – 10.0
Co...........0.5 – 2.5
W............0.2 – 1.0
C........0.05 – 0.15
Si............ 1.0 max.
Mn.......... 1.0 max.
P...........0.04 max.
S...........0.03 max.
Cr......20.5 – 23.0
Fe...... 17.0 – 20.0
Mo....... 8.0 – 10.0
Co...........0.5 – 2.5
W............0.2 – 1.0
C........0.05 – 0.15
Si............ 1.0 max.
Mn.......... 1.0 max.
P...........0.04 max.
S...........0.03 max.
PHYSICAL CONSTANTS AND THERMAL PROPERTIES
Density, Ib/in3..........................................................................0.297
g/cm3......................................................................... 8.22
Melting Point, °F......................................................2300 – 2470
°C......................................................1260 – 1355
Specific Heat, Btu/lb •°F.....................................................0.110
J/kg •°C........................................................... 461
Permeability at 200 Oersted (15.9 kA/m).................. 1.0110
Coefficient of Expansion, 70 – 200°F, 10-6 in/in •°F........ 7.4
20 – 100°C, μm/m •°C.......... 13.3
Thermal Conductivity, Btu • in/ft2• h•°F........................... 80.4
W/m•°C........................................... 11.6
Electrical Resistivity, ohm • circ mil/ft.............................. 698
μΩ•m................................................. 1.16
g/cm3......................................................................... 8.22
Melting Point, °F......................................................2300 – 2470
°C......................................................1260 – 1355
Specific Heat, Btu/lb •°F.....................................................0.110
J/kg •°C........................................................... 461
Permeability at 200 Oersted (15.9 kA/m).................. 1.0110
Coefficient of Expansion, 70 – 200°F, 10-6 in/in •°F........ 7.4
20 – 100°C, μm/m •°C.......... 13.3
Thermal Conductivity, Btu • in/ft2• h•°F........................... 80.4
W/m•°C........................................... 11.6
Electrical Resistivity, ohm • circ mil/ft.............................. 698
μΩ•m................................................. 1.16
TYPICAL MECHANICAL PROPERTIES
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SHANGHAI KANGSHENG AVIATION MATERIALS TECHNOLOGY CO., LTD.
Address: No. 5999, Huyi Road, Waigang Town, Jiading District, Shanghai
Tel：13641813331
Technical support：13671903676
Emial：ksalloy@ksalloy.com
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