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Source control and specification control drawings. |
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|  MIL-W-64044 (AR)
4.5.3 Umbilical lead pull test. Apply the required pull at
the connector. The umbilical lead shall withstand a pull of 5.0
lbs. minimum without displacing the cable stop eyelet. Any nose
cone assembly that does not comply with the drawing requirement
shall be classed defective.
5.
PACKAGING
5.1 Packaginq and marking. The warhead parts and assemblies
shall be packaged and marked in accordance with MIL-STD-1169.
5.2 Packing and marking. The packaged parts and assemblies
shall be packed and marked in accordance with MIL-STD-1169.
5.3 Ammunition data cards.
Data card information shall be as
specified in MIL-STD-1167.
6.
NOTES
6.1 Intended use. The assemblies and components covered by
this specification are intended for use as part of the 2.75 Inch
Folding Fin Aerial Rocket System.
6.2 Ordering data.
See MIL-A-48078.
6.3 Submission of ins pection equi pment for design app rovals.
See 6.2 of MIL-A-48078. Submit designs as required to Commander,
US Army Armament Research and Development Command, ATTN:
DRDAR-QAF-I, Dover, NJ 07801.
6.4 First article. When a first article is required for
inspection and approval, see 3.3 and 4.3.
Source control and specification control drawings.
6.5
Certificates of conformance from the supplier certifying that the
item complies with the drawing requirements shall be provided to
the Government representative.
Preparing activity:
Custodian:
Army-AR
Army-AR
(Project 1340-A646)
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