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Table II. Conditioning temperature
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Thruster, Cartridge Actuated, M13 Assembly
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Air Force packaging



MIL-T-46604B
a. Cartridge, Impulse, M119
P/N 8595513
b. O-ring
MS29513-19
c. Plug, protective
MIL-C-5501/10-F5
d. Body
P/N 10520976
e. O-ring
MS29513-15
f. Piston and Pellet Assembly
P/N 10520979
g. Setscrew (2 each)
Commercial
h. Ring
P/N 10520489
i. Cap, protective
MIL-C-5501/9-F9
j. Piston Fastener and Pellet Assembly
P/N 10520980
k. Pin, shear, piston (2 each)
P/N 10520487
l. O-ring (2 each)
MS29513-14
m. Breech
P/N 10520977
n. Pin, firing P/N 10520978
o. O-ring
MS29513-115
p. O-ring
MS29513-9
q. Pin, shear, firing pin
P/N 10520486
r. Base cap and Pellet assembly
P/N 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 65F, 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.
9

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