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MIL-L-48063A(MI)
4,4.14.2 High temperature test. The launcher assembly without shipping
covers shall be subjected to high temperature as specified in MIL-STD-81O,
Method 501, Procedure I. Immediately upon completion of the environmental
conditioning, the sample shall be visually examined for damage or defects
and the following tests shall be performed:  Simulated firing, insulation
resistance and continuity.
4.4.14.3 Low temperature test.  The launcher assembly without shipping
covers shall be subjected to low temperature of -54C (-65F) for 24 hours
as specified in MIL-STD-81O, Method 502. Immediately upon completion of the
environmental conditioning, the sample shall be visually examined for damage
or defects and the following tests shall be performed: Simulated firing,
insulation resistance and continuity.
4.4.14.4 Shock test. The launcher assembly without shipping covers,
shall be mounted on a bomb rack, loaded with seven (7) inert 2.75 Inch FFAR
and subjected to shock in the vertical and longitudinal axis in accordance
with MIL-STD-81O, Method 516, Procedure I. The vertical half sine shock
pulses shall have a peak of 10.0 g's and an 18 ms duration, and the
longitudinal half sine shock pulses shall have a peak of 13.5 g's and an
18 ms duration. The applied shock shall be measured midway between the
attachment lugs on the bomb rack. The inert rockets shall not be released
during the shock test. This test shall be performed with the intervalometer
in the arm position with no power applied. Upon completion of the above,
the sample shall be visually examined for damage or defects, and
intervalometer advancement. The following tests shall be performed:
Simulated firing, insulation resistance, continuity, detent operations
and loading.
4.4.14.5 Vibration.  The launcher loaded with seven (7) inert 2.75
Inch FFAR shall be subjected to vibration as specified in MIL-STD-810,
Method 514, Procedure I, Curve C. Electrical contact between the launcher
and each rocket motor shall be monitored continuously during the vibration,
The following tests will be performed during a resonant dwell and at the
end of vibration in each axis: Simulated Firing examination for inter-
valometer advancement. The inert rocket shall not be released during the
vibration test. Immediately upon completion of the environmental
conditioning, the following tests shall be performed: Visual examination
for damage or defects and for intervalometer advancement, Simulated
Firing Test, Continuity, Insulation Resistance and Detent Operation.
4.4.16.6 Rough handling. The launcher shall be fully loaded with
2.75 Inch FFAR Rockets and shipping covers in place. The launcher shall
be dropped four times onto a solid concrete surface, falling freely through
a vertical distance of 30 1 inch and striking at an angle of 45 degrees
1 degree. The 30 inch distance shall be measured from the lowest point
on the launcher, when in the 45 degree attitude, to the solid concrete
surface. The forward end of the launcher is to strike the concrete
on two of the drops, and the aft end on the other two drops. Subsequently,
30

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