NCK 20 TA (France / AIR) Material Properties
Material group:
Nonferrous Alloys / Nickel / Nickel Alloys
Country/Standard:
France / AIR
Data updates
Latest Update: 2018-12
Total number of updates: 1
Update History:
Mechanical Properties
Temperature
Physical Properties
Temperature
Composition
CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
1.00 – 2.00
UNIT
%
CAS NUMBER
7429-90-5
CRITERIA
B
VALUE
≤ 0.02
UNIT
%
CAS NUMBER
7440-42-8
CRITERIA
C
VALUE
≤ 0.13
UNIT
%
CAS NUMBER
7440-44-0
CRITERIA
Co
VALUE
val1
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UNIT
%
CAS NUMBER
7440-48-4
CRITERIA
Cr
VALUE
val1
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UNIT
%
CAS NUMBER
7440-47-3
CRITERIA
Cu
VALUE
val1
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UNIT
%
CAS NUMBER
7440-50-8
CRITERIA
Fe
VALUE
val1
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UNIT
%
CAS NUMBER
7439-89-6
CRITERIA
Mn
VALUE
val1
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UNIT
%
CAS NUMBER
7439-96-5
CRITERIA
Ni
VALUE
val1
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UNIT
%
CAS NUMBER
7440-02-0
CRITERIA
P
VALUE
val1
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UNIT
%
CAS NUMBER
7723-14-0
CRITERIA
Pb
VALUE
val1
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UNIT
%
CAS NUMBER
7439-92-1
CRITERIA
S
VALUE
val1
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UNIT
%
CAS NUMBER
7704-34-9
CRITERIA
Si
VALUE
val1
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UNIT
%
CAS NUMBER
7440-21-3
CRITERIA
Ti
VALUE
val1
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UNIT
%
CAS NUMBER
7440-32-6
AIR 9165: 1973 / General conditions for delivery and use of heat-resistant wrought steels and alloys used in aeronautical structures
Heat Treatments
- <b>Heat treatment 1: </b> <br> 1080°C, 8h, air <br> 710°C, 16h, air <br> <b>Heat treatment 2: </b> <br> 1050-1080°C, 8h, air <br> <b>Heat treatment 3: </b> <br> 1050-1080°C, 8h, air <br> 710°C, 16h, air <br> <b>Heat treatment 4: </b> <br> 1100-1150°C, air <br> <b>Heat treatment 5: </b> <br> 1100-1150°C, air <br> 710°C, 16h, air <br>
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13 Cross References
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14 Composition
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14 Mechanical Properties
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3 Physical Properties
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1 Heat Treatment
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- Metallography
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- Machinability
-
- Stress-Strain
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1 Formability
-
- Fatigue
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- Fracture
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2 Creep
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- Joints
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- Coatings
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- Dimensions
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- Tribology
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- Corrosion
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- Ageing
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- Weatherability
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- Irradiation
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5 Total Suppliers