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Carbon		0.08 - 0.16
Chromium		20 - 22.5
Cobalt		18.5 - 21
Iron		Balance
Manganese		1 - 2
Molybdenum		2.5 - 3.5
Nickel		19 - 21
Niobium+Tantalum		0.75 - 1.25
Nitrogen		0.1 - 0.2
Phosphorus		0.04 max
Silicon		1 max
Sulphur		0.03 max
Tungsten		2 - 3

Principal Design Features		This iron based alloy has a long history, back to 1950, of high strength at temperatures up to 1500 F and is capable of sustaining moderate loading at temperatures of 2000 F. It has good oxidation resistance at high temperature and also possesses good corrosion resistance to sulfuric acid (at room temperature) and to nitric acid. High temperature strength derives directly from the chemical composition of the alloy and is not dependent upon age hardening.

Applications		Industrial furnace structural parts and fixtures. High temperature bolts and gas turbine combustion chambers, exhaust manifolds, and turbine blades.

Machinability		Similar to the austenitic (300 series) stainless steels in machining characteristics the alloy can be machined by conventional means. Both carbide and high speed tool steels may be used for turning or boring. However high speed steels work best for drilling and milling operations.

Forming		Forming by cold working is preferred and the alloy has good ductility. It does work harden and may require a solution heat treatment to restore ductility during cold forming.

Welding		Multimet is readily weldable by resistance, MIG and TIG process. As is true of the high temperature alloys in general submerged-arc welding should not be used because the high heat input of that process may cause cracking in the weld area. Matching composition filler metal should be used and for multi-pass welds each bead should be allowed to cool to touch before the next bead is started. Pre or post-heating is not required.

Heat Treatment		Solution heat treat at 2150 F followed by water quench or rapid air cool.

Forging		Hot forging is done by heating the billet to 2150 F, allowing adequate time for through heating. Forging should stop before the temperature drops below 1700 F. Re-heat for additional forging if necessary.

Hot Working		See the comments under "Forging".

Cold Working		The alloy cold works readily and can be drawn, formed by bending or spinning as it has good ductility. Work hardening occurs and it may be necessary to give the piece a solution heat treatment before finishing all cold working. In finished condition the part should be solution heat treated to restore optimum mechanical properties of the alloy.

Annealing		See "Heat Treatment".

Aging		Not applicable as a strengthening process. Long term use at temperatures in the 1200 F to 1600 F range results in a reduction of impact strength.

Hardening		The alloy can be hardened only by cold working.

Other Physical Props		Impact strength in Charpy tests. Charpy Keyhole Notch Impact Strength. Bar stock, aged at 1200 F, 2 hrs. 57 ft. lbs. at 70 F " " " " " 63 ft. lbs. at 1200 F Charpy V-Notch Impact Strength. Plate, solution annealed 56 ft. lbs. at minus 321 F " " " 86 ft. lbs. at minus 108 F " " " 113 ft. lbs. at 70 F

Physical Data : [top]

Density (lb / cu. in.)	0.296
Specific Gravity	8.2
Specific Heat (Btu/lb/Deg F - [32-212 Deg F])	0.104
Electrical Resistivity (microhm-cm (at 68 Deg F))	558
Melting Point (Deg F)	2450
Poissons Ratio	0.298
Thermal Conductivity	101
Mean Coeff Thermal Expansion	8.5

MSO currently has no data available for this grade.