MIL-T-46604B
a. Cartridge, Impulse, M119 PIN 8595513 b. 0-ring MS29513-19
c. Plug, protective MIL-C-5501I10-F5 d. Body PIN 10520976
e. 0-ring MS29513-15
f. Piston and Pellet Assembly PIN 10520979 g. Setscrew (2 each) Commercial
h. Ring PIN 10520489
i. Cap, protective MIL-C-5501I9-F9 j. Piston Fastener and Pellet Assembly PIN 10520980
k. Pin, shear, piston (2 each) PIN 10520487 l. 0-ring (2 each) MS29513-14 m. Breech PIN 10520977 n. Pin, firing PIN 10520978
o. 0-ring MS29513-115 p. 0-ring MS29513-9
q. Pin, shear, firing pin PIN 10520486 r. Base cap and Pellet assembly PIN 10520975
4.3.4 Functional.
4.3.4.1 Ballistics. The test sample shall be rigidly supported so that the entire thrust is borne by the thruster mounting points. The samples shall be tested within 10 minutes after removal from the temperature conditioning chamber. When this time limit is exceeded, the sample units shall be reconditioned at the original temperatures.
4.3.4.2 Temperature conditioning. Each assembled thruster shall be conditioned for not less than 4 hours nor greater than 24 hours. When reconditioning thrusters at •65•F, all condensation shall be removed from the exterior surfaces before returning the thruster to the conditioning chamber.
4.4 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 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 8836128 and 8836129. Level B shall be in accordance with Drawings 8836128 and 9217388.
5.1.1 Lot numbers. Lot numbers shall be in accordance with MIL-STD-1168.
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