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Family Owned and Managed - Making Stainless Steel Plate and Nickel Alloy Plate Products Since 1952
Sandmeyer Steel
Specification Sheet: Alloy 800, 800H and 800AT
Nickel-Iron-Chromium Alloy 800 (UNS N08800), Alloy 800H (UNS N08810), and
Alloy 800AT (UNS N08811) are Designed to Resist Oxidation and Carburization

Applications | Standards | Corrosion Resistance | Chemical Analysis
Mechanical Properties | Physical Properties | Oxidation Resistance
Heat Treatment | Cold Formability | Welding

 

Click here to download Alloy 800 PDF file

Alloy 800 (UNS N08800), Alloy 800H (UNS N08810), and Alloy 800AT (UNS N08811) are nickel-iron-chromium alloys designed to resist oxidation and carburization at elevated temperatures. The nickel content, 32%, makes the alloys highly resistant both to chloride stress-corrosion cracking and to embrittlement from precipitation of sigma phase. The general corrosion resistance is excellent. In the solution annealed condition, Alloys 800H and 800AT have superior creep and stress rupture properties. All three versions of the basic Alloy 800 have been approved as materials of construction under ASME Boiler and Pressure Valve Code, Section I-Power Boilers, Section III-Nuclear Vessels, and Section VIII-Unfired Pressure Vessels.

Alloy 800, Alloy 800H and Alloy 800AT are identical except for the higher level of carbon (0.05 to 0.10 percent) in Alloy 800H, and the addition of up to 1.00 percent aluminum + titanium in Alloy 800AT. Alloy 800 is normally used in this service at temperatures to approximately 1100°F (593°C). Alloy 800H and Alloy 800AT are normally used above approximately 1100°F where resistance to creep and rupture is required.


Applications

  • Chemical and petrochemical processing equipment
  • Power generation
  • Thermal processing fixtures
  • Steel production

 

Standards
ASTM........... B 409
ASME.......... SB 409
AMS ........... 5871

 

Corrosion Resistance
The chromium and nickel contents of Alloys 800, 800H and 800AT are higher than those of the familiar Type 304 stainless steel alloy. Under many conditions of service, the performance of Alloys 800, 800H, 800AT and Type 304 are similar. For example, comparable behavior can be expected in most rural and industrial atmospheres and in chemical media such as nitric acid and organic acids. Neither Alloys 800, 800H and 800AT nor Type 304 are suggested for sulfuric acid service except at lower concentrations and temperatures. Like the austenitic stainless steels, Alloys 800, 800H and 800AT are subject to sensitization (precipitation of chromium carbides at grain boundaries) if heated for excessive time in the 1000°-1400°F (538°-760°C) temperature range. The sensitized metal may be subject to intergranular attack by certain corrosive agents including pickling acids or the boiling 65% nitric acids (Huey) test.

Alloy 800 is highly resistant, although not totally immune, to stress-corrosion cracking. In extensive field experience, Alloy 800 has shown excellent service performance in many types of equipment in the petroleum, chemical, food, and pulp and paper industries. Thus, Alloy 800 may offer a distinct advantage for use in moderately corrosive environments where service experience has indicated a tendency toward stress-corrosion cracking of other austenitic stainless steels. However, the alloy is not immune to stress-corrosion cracking as judged by the extremely severe magnesium chloride test.

 

Chemical Analysis
Typical Analysis (Weight %)

  C Mn P S Si Cr Ni Ti Al Ti + Al Cu
Alloy 800 0.02 1.00 0.020 0.010 0.35 21.0 32.0 0.40 0.40 0.30
Alloy 800H 0.08 1.00 0.020 0.010 0.35 21.0 32.0 0.40 0.40 0.30
Alloy 800AT 0.08 1.00 0.020 0.010 0.35 21.0 32.0 1.00 0.30

 

Mechanical Properties
Typical room temperature mechanical properties of Alloys 800, 800H and 800AT are shown. Alloy 800 was annealed at 1800°F (928°C) and Alloys 800H and 800AT were annealed at 2100°F (1149°C). The different anneal temperature used contributed to the difference in strength of the materials.

Mechanical Properties of Alloy 800

Test Temperature 0.2 Offset
Yield Strength
Ultimate
Tensile Strength
Percent
Elongation
°F °C psi (MPa) psi (MPa)  
70 21 43,000 295 87,700 600 44
200 93 39,700 274 81,700 563 43
500 260 34,000 234 76,200 525 39
800 427 33,300 230 74,600 514 40
1000 538 31,700 219 72,000 496 39
1200 649 29,000 200 54,000 372 56
1400 760 22,600 156 32,100 221 85
1500 816 14,200 98 24,800 171 91

Mechanical Properties of Alloy 800H and Alloy 800AT

Test Temperature 0.2 Offset
Yield Strength
Ultimate
Tensile Strength
Percent
Elongation
°F °C psi (MPa) psi (MPa)  
70 21 29,000 200 77,000 531 52
200 93 24,100 166 71,000 490 53
600 316 19,000 131 66,600 459 53
800 427 18,100 125 65,800 454 53
1000 538 16,500 114 63,500 438 51
1200 649 14,800 102 55,700 384 50
1400 780 14,400 99 32,300 223 78
1600 871 11,600 80 18,600 128 120
1800 982 8,900 61 10,200 70 120

Short Time Elevated Temperature Properties
The above tables illustrate the short time high-temperature tensile properties of Alloys 800, 800H and 800AT. The strength of Alloys 800H and 800AT is lower because the heat treatment of Alloys 800H and 800AT at 2100°F (1149°C) results in a larger grain size to provide better creep and stress rupture resistance. The 1800°F (982°C) anneal of Alloy 800 results in a finer grain size to provide better cold formability.

 

Physical Properties
Density :
0.29 g/cm3 (8.03 lbs/in3)

Electrical Resistivity:
99 Microhm-cm    at 70 °F (21 °C)

Magnetic Permeability
<1.02

Specific Heat :
(32°-212 °F)          0.12 Btu/lb-°F
(0°-100 °C)            500 Joules/kg-°K

Linear Mean Coefficient of Thermal Expansion

Temperature Range µm / °F µm / °C
°F °C
70-200 21-93 7.9 14.2
70-300 21-149 8.4 15.1
70-400 21-204 8.6 15.5
70-500 21-260 8.8 15.8
70-600 21-316 9.0 16.2
70-800 21-427 9.2 16.6
70-1000 21-538 9.4 16.9
70-1200 21-649 9.6 17.3
70-1400 21-760 9.9 17.8

Thermal Conductivity

Temperature Range BTU / h-ft °F W / m / °K
°F °C
70 21 6.7 11.6
70-800 21-427 10.6 18.3
70-1800 21-982 17.8 30.8

 

Oxidation Resistance
The alloys are particularly well suited for high temperature applications such as furnace parts and related heating equipment, for petrochemical reforming units and isocracker tubs, and for handling superheated steam in nuclear and conventional power plants. With the specified high levels of chromium and nickel, the alloys offer superior resistance to oxidation and scaling, and to carburization as well.

The following oxidation data for Alloy 800 was obtained by exposing samples to the indicated temperature for 100 hours in still air and cooling. In general, total weight gains greater than 10mg/cm2 indicate that additional exposure at these temperatures will lead to failure.

Since oxidation rates are greatly affected by heating and cooling rates as well as by the atmospheres involved, this data can only be used as approximate guidelines.

100 Hour Still Air Continuous Oxidation Tests

Alloy  Sample Weight Gain (mg / cm2 )
1700°F
(927°C)
1800°F
(982°C)
1900°F
(1038°C)
2000°F
(1093°C)
2100°F
(1149°C)
Alloy 800 0.77 1.8 2.09 2.1 5.06
Type 309 0.80 1.2 2.1 2.5 4.0
Type 310 0.80 1.1 2.6 3.2 5.2

 

Heat Treatment
The anneal cycle conducted on Alloy 800 is typically in the 1800°-1900°F (982°-1038°C) range. The purpose is to soften the material after forming operations while maintaining a relatively fine grain size.

The heat treatment conducted on Alloys 800H and 800AT is typically in the range of 2050°-2150°F (1121°-1177°C). In addition to softening the material after forming operations, an additional purpose of this heat treatment is the development of larger grains for improved resistance to creep and stress rupture.

 

Cold Formability
Alloys 800, 800H and 800AT exhibit excellent cold forming characteristics normally associated with chromium-nickel stainless steels. The high nickel content prevents the austenite to martensite transformation which can occur when Type 301 or Type 304 are cold worked. The alloy has a lower work hardening rate than Types 301 or 304 and can be used in multiple drawn forming operations where relatively large amounts of deformations occur between anneals.

As a consequence of the anneal cycle used on Alloys 800H and 800AT, the large grain size produces a visibly undulated surface called “orange peel” after forming.

 

Welding
Alloys 800, 800H and 800AT can be joined by tungsten arc (GTAW), gas consumable electrode (MIG), or by stick electrode welding techniques commonly used on stainless steels. A number of welding rods and wires are commercially available for joining the alloys. Since these alloys form tightly adhering scales, which can be removed only by grinding, inert gas shielding is desirable.

 

NOTE
This technical data and information represents our best knowledge at the time of printing. However, it may be subject to some slight variations due to our ongoing research program on corrosion resistant grades. We, therefore, suggest that information be verified at time of inquiry or order. Furthermore, in service, real conditions are specific for each application. The data presented here is only for the purpose of description and may only be considered as guarantees when our Company has given written formal approval.

 

 

 

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