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nickel 200 super alloys [al 200 (tm),ametek 899l (tm),ametek 899m (tm),nickelvac 200 (tm),vdm nickel 99.2 (tm)] material property data sheet

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Metal Suppliers Online: Material Property Data

Super Alloy Nickel 200

 


Specifications

The following specifications cover Super Alloy Nickel 200

  • ASTM B160
  • ASTM B161
  • ASTM B162
  • ASTM B163
  • ASTM B366
  • ASTM B725 (Pipe- Welded)
  • ASTM B730
  • DIN 2.4060
  • DIN 2.4066
  • UNS N02200

 

 


Property Results

Related Metals:


Chemistry Data : [top]

Carbon 0.15 max
Copper 0.25 max
Iron 0.4 max
Manganese 0.35 max
Nickel Balance
Silicon 0.35 max
Sulphur 0.01 max


Principal Design Features Commercially pure (99%) wrought nickel, basically unalloyed but containing minor amounts of other elements usually totaling less than 1%.

Applications Electronic parts, resistance to corrosion applications such as handling alkaline solutions and foods.

Machinability Commercially pure nickel is soft and "gummy" to machine. However it can be machined with standard tooling. High-speed-steel tools work better than carbide tooling and it is important to maintain a high positive rake angle on cutting tools.

Forming Nickel is readily formed by all of the conventional means. It behaves in a similar fashion to plain carbon steel, except that more power is required to form nickel.

Welding All of the conventional welding and joining methods work with nickel. In particular the shielded metal-arc, gas tungsten-arc and gas metal-arc welding methods are recommended. Use nickel filler wire or electrodes.

Heat Treatment Anneal at 1500 F to 1300 F and air cool.

Forging Forging may be done at 2250 F to 1700 F.

Hot Working Hot working may be done in the range of 2200 F to 1200 F.

Cold Working Cold working may be accomplished using standard tooling as for plain carbon steels. More power is required as the nickel material has a higher elastic limit than steel and thus resists deformation.

Annealing Annealing at 1500 F as a typical temperature. Annealing may be done within the range of 1700 F to 1300 F depending upon the degree of cold working and time at temperature.

Hardening Hardens due to cold working only.

Physical Data : [top]

Density (lb / cu. in.) 0.321
Specific Gravity 8.89
Specific Heat (Btu/lb/Deg F - [32-212 Deg F]) 0.109
Electrical Resistivity (microhm-cm (at 68 Deg F)) 76
Melting Point (Deg F) 2625
Poissons Ratio 0.29
Thermal Conductivity 463
Mean Coeff Thermal Expansion 7.4
Modulus of Elasticity Tension 29.7


Mechanical Data : [top]

Form Plate
Condition Hot Rolled
Temperature 70
Tensile Strength 77
Yield Strength 50
Elongation 45
Rockwell B67

Form Plate
Condition Hot Rolled Annealed
Temperature 70
Tensile Strength 67
Yield Strength 52
Elongation 50
Rockwell B60

Form Sheet
Condition Test Specimen Annealed
Temperature 70
Tensile Strength 65
Yield Strength 22
Elongation 47

Form Strip
Condition Annealed
Temperature 70
Tensile Strength 65
Yield Strength 22
Elongation 47

Form Strip
Condition Spring Temper
Temperature 70
Tensile Strength 110
Yield Strength 93
Elongation 8


[top]
Nickel - www.nidi.org

Copper - www.copper.org

Titanium - www.titanium.org

Steel Lynx - www.mlc.lib.mi.us/~stewarca/steelynx.html


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