MIL-DTL-60584B (AR)
3.6 Air pressure test. Each assembly shall withstand an internal air pressure in
accordance with requirements specified on drawing 10542946 without evidence of leakage.
3.7 Ballistic testing. The projectile assembly shall reveal no evidence of metal parts
failure. Metal parts failure shall be:
a. Loss or breakup of metal parts components in flight.
b. Loss or fanning of the rotating band.
c. Shear of rotating band as evidenced by complete lack of engraving.
3.8 Workmanship.
3.8.1 Painting. Painting shall comply with the requirements of drawing 10542945 . All
paint shall be dry to the touch before packing for shipment. Drying time prior to testing shall be
in accordance with the applicable specification or drawing. Painting shall be complete, void
free, and undamaged.
3.8.2 Surface finish. The requirements for surface finish are as detailed on the applicable
drawing. The roughness comparison specimens prescribed by ASME B46.1 shall be used as a
basis for surface roughness determinations, except in press fit area.
3.8.3 Threads. Threads shall be full and undamaged for the entire minimum length or
depth as specified on drawing 10542945.
3.8.4 Burr. No part shall have a burr which might interfere with the assembly or function
of the round or which might be injurious to personnel handling the item.
3.8.5 Foreign matter. No part or assembly shall contain dirt, grease, chips, rust, corrosion
or other foreign matter. Particular attention shall be given to the cavity of the metal parts to
assure that no grit, scale or other foreign matter remains therein after final cleaning. The
projectile cavity may contain light rust, in the form of discoloration or staining with no visual
evidence of pitting, etching, flaking, or other surface damage, covering not more than 25 percent
of the cavity surface.
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