(Industry association specifications and standards are generally available
for reference from libraries. They are also distributed among technical groups
and using Federal agencies.)
2.3 Order of precedence. In the event of a conflict between the text of
this specification and the references cited herein, the text of this specifica-
tion shall take precedence
3.1 Materials and components.
3.1.1 Materials. All materials cited on TDPL 122-3-60 and on the subsidiary
drawings shall conform to the specifications listed thereon or to the specific
characteristics set forth on the drawings.
3.1.2 Components. All components of the projectile shall conform to the
specifications and drawings listed on TDPL 1.22-3-60.
The projectile shall be assembled as shown on Drawing
3.3.1 Wrap assembly. The wrap assembly shall have a maximum yield force of
24.25 pounds and a maximum yield strain of .039 inch per inch (in/in) when
tested in accordance with 188.8.131.52.
3.3.2 Integrity/accuracy. When fired from a launcher, the projectile shall
have no separation of the breakband from the projectile prior to target impact
and shall maintain sufficient accuracy to strike a 46 centimeter (cm) wide, 175
cm high target at a distance of 40.0 + 0.5 meter from the launcher when tested
in accordance with 184.108.40.206.
3.5 Preproduction. Prior to the start of regular production, a preproduc-
tion sample of components shall be produced in accordance with this specifica-
tion for examination and test (see 4.3).
3.6 Workmanship. The projectile body shall be free from imperfections
listed in Table I of MIL-STD-407 and damage such as rips or tears which could
affect its intended use.
QUALITY ASSURANCE PROVISIONS
4.1 Responsibility for inspection.
4.1.1 Contractor's responsibility. Unless otherwise specified in the con-
tract or purchase order, the contractor is responsible for the performance of
all inspection requirements as specified herein. Except as otherwise specified