---

Aluminum		0.75 - 1.5
Carbon		0.09 max
Chromium		16 - 18
Iron		Balance
Manganese		1 max
Nickel		6.5 - 7.75
Phosphorus		0.04 max
Silicon		1 max
Sulphur		0.04 max

Principal Design Features		A precipitation hardenable chromium-nickel-aluminum stainless steel combining high strength, moderate corrosion resistance and properties well suited for flat springs.

Applications		Used for applications requiring good strength, corrosion resistance and mechanical properties up to 800 F in service. It is often used for very detailed, intricate parts due to its low distortion in heat treatment. Very stable. Commonly found in a variety of springs and washers.

Machinability		Rated at 75 % of B1112. This alloy displays long gummy chips that require chip breakers to overcome. Slow speeds and constant feeds are recommended for best results.

Forming		Forming characteristics of this alloy are similar to 301 stainless steel. Intermediate annealing may be necessary for radical forming operations.

Welding		Most common arc and resistance methods have been successfully employed with 17-7 PH. It is recommended that inert gas shielding be employed during fusion welding to reduce the oxidation of aluminum during the process. Pre-heating and post-weld annealing are not necessary with this alloy.

Heat Treatment		CONDITION C - Results from heavy cold working (generally 45-50% reduction) of solution treated material. CONDITION CH900- Heat Condition C material to 900 F(482 C), hold for 1 hour, air cool. CONDITION A1750- After fabrication, heat solution treated material to 1750 F(955 C), hold for 10 minutes, cool rapidly to room temperature. CONDITION R100- Within 1 hour of treating to Condition A1750, cool to -100 F(-73 C) and hold for 8 hours. Air warm to room temperature. CONDITION RH 950- From Condition R100 material, heat to 950 F( 510 C), hold for 90 minutes, air cool. CONDITION T- After fabrication, heat to 1400 F (760 C) and hold for 90 minutes. Within 60 minutes, cool to 55 F (13 C), and hold for 1/2 hour. CONDITION TH1050- From Condition T, heat to 1050 F (565 C) and hold for 90 minutes, air cool

Cold Working		In Condition A, this material can be easily formed using most common procedures.

Annealing		1950 F (1066 C) for 3 minutes for each .1 inch (2.5 mm) of thickness, air cool.

Aging		Solution anneal at 2150 F for 4 hours and air cool. Follow with 1975 F for 4 hours and air cool, then 1550 F for 24 hours, air cool and 1400 F for 16 hours, air cool to complete precipitation hardening process. Resistant to liquid oxygen and hydrogen and ammonia. For optimum performance, material must be clean and free of scale and impurities.

Physical Data : [top]

Density (lb / cu. in.)	0.282
Specific Gravity	7.81
Specific Heat (Btu/lb/Deg F - [32-212 Deg F])	0.11

Form		Sheet
Condition		A 1750
Temper		70
Tensile Strength		132
Yield Strength		40
Elongation		20
Rockwell		B85
Form		Sheet
Condition		Annealed
Temper		70
Tensile Strength		130
Yield Strength		45
Elongation		30
Rockwell		B85
Form		Sheet
Condition		C
Temper		70
Tensile Strength		219
Yield Strength		191
Elongation		5
Rockwell		C43
Form		Sheet
Condition		CH 900
Temper		70
Tensile Strength		265
Yield Strength		259
Elongation		3
Rockwell		C49
Form		Sheet
Condition		R 100
Temper		70
Tensile Strength		174
Yield Strength		115
Elongation		10
Rockwell		C37
Form		Sheet
Condition		RH 950
Temper		70
Tensile Strength		220
Yield Strength		200
Elongation		9
Rockwell		C46
Form		Sheet
Condition		T
Temper		70
Tensile Strength		145
Yield Strength		99
Elongation		10
Rockwell		C31
Form		Sheet
Condition		TH 1050
Temper		70
Tensile Strength		190
Yield Strength		160
Elongation		10
Rockwell		C42