MIL-DTL-50699B
h. O-ring, MS28775-009
i. Mounting Bracket, P/N 11731741
4.6.7 Ignition device sensitivity. Drop test a sample of ignition devices, assembled and crimped
into the retainer, selected in accordance with table II. Use a steel ball 15/16 inches in diameter and
weighing 1.94 ± 0.02 ounces at a drop height of 13 inches (measured from bottom of suspended ball to top
of firing pin) in a primer sensitivity machine approved by the procuring agency.
4.6.8 Functional.
4.6.8.1 Ballistics. The test sample shall be rigidly supported in the fixture and fired by a source
delivering an output of 700 +25, -0 psig at 70 ± 5°F. The sample shall be tested within 5 minutes after
removal from the temperature conditioning chamber. When this time limit is exceeded, the sample units
shall be reconditioned in accordance with 4.6.8.2. Required pressure readings shall be taken as specified
in 3.8.1.
4.6.8.2 Temperature conditioning. Each assembled initiator shall be conditioned for not less than
4 hours nor greater than 24 hours. When reconditioning initiators at -60°F, all condensation shall be
removed from the exterior surfaces before returning the initiator to the conditioning chamber.
4.7 Inspection of packaging. The sampling and inspection of the packaging, packing, and container
marking shall be in accordance with section 5.
5. PACKAGING
5.1 Packaging. For acquisition purposes, the packaging requirements shall be as specified in the
contract or order (see 6.2). When packaging of materiel is to be performed by DoD or in-house contractor
personnel, these personnel need to contact the responsible packaging activity to ascertain packaging
requirements. Packaging requirements are maintained by the Inventory Control Point's packaging
activities within the Military Service or Defense Agency, or within the military service's system
commands. Packaging data retrieval is available from the managing Military Department's or Defense
Agency's automated packaging files, CD-ROM products, or by contacting the responsible packaging
activity.
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 initiator assembly is used in conjunction with other propellant actuated
devices in Aircrew Emergency Escape Systems. Since the initiator was designed specifically for military
use, there is no commercial application.
6.2 Acquisition requirements. Acquisition documents should specify the following:
a. Title, number, and revision letter of this specification
b. Issue of DODISS to be cited in the solicitation and, if required, the specific issue of individual
documents referenced (see 2.1.1 and 2.1.2)
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