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| MIL-T-46632B(OS)
4.6.3 Structural strength. The thruster shall be subjected to the structural strength test
in accordance with the requirements of 3.6.
4.6.4 Shear pin strength. After application of protective finish, the pin shall be subjected
to the shear pin strength test to determine compliance with 3.7. The test shall be performed in
a fixture in conjunction with a tensile testing machine.
4.6.5 Breakaway torque. A torque wrench capable of measuring the torque requirements
specified in 3.5.2 shall be used with an appropriate adapter to determine the adequacy of the
joints. The thruster body shall be secured and the torque applied to the holding ring.
4.6.6 Protective finish. Test procedures for protective finish shall be in accordance with
the applicable specification referenced on the applicable drawing.
4.6.7 Residual magnetism. The assembly shall be tested for excessive residual magnetism
using an approved compass in an area free of local magnetic effects by placing the assembly 5
inches from the end and at the same height as the compass, in a north-south horizontal position
(cap end at south) with the compass set in an east-west heading. The assembly shall be moved at a
speed no greater than 10 feet per minute past the compass for its entire length, rotated 90 degrees
in the horizontal position about its longitudinal axis and moved slowly back past the compass.
This procedure shall be repeated for each 90 degree rotation of the assembly for four full passes.
4.7 Inspection of packaging. The sampling and inspection of the packaging, packing, and
container marking shall be in accordance with the requirements of section 5.
5. PACKAGING
5.1 Packing and marking. Packing and marking shall be Level A or B, as specified by the
contracting activity (see 6.2). Level A shall be in accordance with Drawings 8797633 and 8797634.
Level B shall be in accordance with Drawings 8797633 and 9235819.
5.2 Air Force packaging. Air Force packaging shall be in accordance with TPO 00-921-5048.
6. NOTES
(This section contains information of a general or explanatory nature that may be helpful but
is not mandatory.)
6.1 Intended use. The thruster assembly is used in conjunction with other propellant actuated
devices in Aircrew Emergency Escape Systems.
6.2 Acquisition requirements. Acquisition documents must specify the following:
a. Title, number, and date of this specification
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