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NPFC - MIL-P-85856/8

POWDER MATERIALS FOR FLAME AND PLASMA SPRAYED COATINGS NICKEL CHROMIUM ALLOY, TYPE I, CLASS 2, COMPOSITION B

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Organization: NPFC
Publication Date: 7 December 1988
Status: active
Page Count: 2
scope:

This specification is approved for use by all Departments and Agencies of the Department of Defense.

The complete requirements for acquiring the powder described herein shall consist of this document and the latest issue of MIL-P-85856.

Chemical Composition

Cr Ni Fe C Mn Si O2 ---------------------------------------------- 18.0 76.0 1.0 0.25 2,5 1.5 (1) 21.0 80.0 max. max. max. max.

Particle Size/Distribution +120 Mesh (+125 µm) 1.0 max. +140 Mesh (+106 µm) 10.0 max. +325 Mesh (+45 µm) 80.0 min. Sprayed Coating Properties Bond Strength 31.0 MPa (4500 psi) min. Hardness Rockwell 15T, 90 min. Microstructure See paragraph 4.5.4.1.2 Porosity - 15% max. Unmelted Particles - 15% max.

Deposit Efficiency and Deposition Rate

70% min for N2/H2 @ 19.0 lb/hr 60% min for A/H2 @ 19.0 lb/hr

Comparable Documents

Powder which meets the requirements specified is qualified under the following specifications.

General Electric Company B5OTF40, Class A Pratt & Whitney Aircraft PWA 1315 Rolls-Royce, Ltd. MSRR 9507/8

Document History

September 4, 1998
POWDER MATERIALS FOR FLAME AND PLASMA SPRAYED COATINGS NICKEL CHROMIUM ALLOY, TYPE I, CLASS 2, COMPOSITION B
A description is not available for this item.
October 29, 1991
POWDER MATERIALS FOR FLAME AND PLASMA SPRAYED COATINGS NICKEL CHROMIUM ALLOY, TYPE I, CLASS 2, COMPOSITION B
A description is not available for this item.
MIL-P-85856/8
December 7, 1988
POWDER MATERIALS FOR FLAME AND PLASMA SPRAYED COATINGS NICKEL CHROMIUM ALLOY, TYPE I, CLASS 2, COMPOSITION B
This specification is approved for use by all Departments and Agencies of the Department of Defense. The complete requirements for acquiring the powder described herein shall consist of this...

References

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