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nitronic 33(tm) super alloy material property data sheet - product availability and request a quote

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Super Alloy Nitronic 33(tm)


Availability

Super Alloy Nitronic 33(tm) is stocked by 0 North American distributors and produced by 9 large mills. Distributors will offer small quantity buys while mills will generally only sell large quantities, with delivery times anywhere from 10 to 50 weeks depending on size and form required

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Specifications

The following specifications cover Super Alloy Nitronic 33(tm)

  • ASTM A240 (XM-29)
  • ASTM A249 (XM-29)
  • ASTM A269 (XM-29)
  • ASTM A276
  • ASTM A312 (XM-29)
  • ASTM A412 (XM-29)
  • ASTM A479 (XM-29)
  • ASTM A580 (XM-29)
  • ASTM A688 (XM-29)
  • ASTM A813 (TP XM-29)
  • ASTM A814 (TP XM-29)
  • UNS S24000

Property Results

Chemistry Data : [top]

Carbon

0.08 max

Chromium

17 - 19

Iron

Balance

Manganese

11.5 - 14.5

Nickel

2.25 - 3.75

Nitrogen

0.2 - 0.4

Phosphorus

0.06 max

Silicon

1 max

Sulphur

0.03 max


Principal Design Features Designed primarily for low magnetic permeability, high yield strength and strong cryogenic properties.

Applications A wide variety of cryogenic equipment including pipe and tube assemblies, valves, tanks and cable typify the applications of this alloy. It has also found use in a number of rotating parts such as fans and containment rings.

Machinability Slow speeds, positive feeds and abundant resulphurized lubricant are essential to success in machining this alloy. Speeds and feeds similar to those employed with 316 or 317 stainless are appropriate here. All common machining practices can be used on this material. Chips will be tough and stringy and it is recommended that curlers or breakers are used.

Forming All common forming techniques can be used with this alloy. Springback will be greater than with standard austenitics and should be taken into consideration when choosing the appropriate forming forces. Process annealing is recommended to remove stresses resulting from this alloys' high work hardening rate. Heat to 1950 F(1065 C) for intermediate anneal.

Welding Pre-heating is not required with this material and all common welding methods including gas tungsten arc, gas metal arc and submerged arc are acceptable. Filler metal selection should be of similar chemistry for maximum strength and resistance to intergranular attack.

Forging Heat to 2000 F, soak to equalize, then heat to 2150 and equalize prior to forging.

Annealing Soak at 1900-2050 F, quench quickly in air or water.

Hardening Hardening this alloy requires cold working. It will not harden with exposure to thermal treatment.

Physical Data : [top]

Density (lb / cu. in.) 0.28
Specific Heat (Btu/lb/Deg F - [32-212 Deg F]) 0.11
Poissons Ratio 0.298
Modulus of Elasticity Tension 29


Mechanical Data : [top]

Form

Sheet

Condition

Annealed

Temper

70

Tensile Strength

115

Yield Strength

66

Elongation

49

Rockwell

B95


Form

Sheet

Condition

Cold Reduced 10%

Temper

132

Tensile Strength

100

Yield Strength

32

Rockwell

C29


Form

Sheet

Condition

Cold Reduced 20%

Temper

159

Tensile Strength

135

Yield Strength

19

Rockwell

C35


Form

Sheet

Condition

Cold Reduced 30%

Temper

185

Tensile Strength

168

Yield Strength

11

Rockwell

C40


Form

Sheet

Condition

Cold Reduced 40%

Temper

202

Tensile Strength

180

Yield Strength

7

Rockwell

C43


Form

Sheet

Condition

Cold Reduced 50%

Temper

210

Tensile Strength

190

Yield Strength

6

Rockwell

C45


Form

Sheet

Condition

Cold Reduced 60%

Temper

223

Tensile Strength

200

Yield Strength

5

Rockwell

C46



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