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|  MIL-T-46692B
to shipment and those defective items shall be removed from the production lot. Film
interpretation of the radiographs shall verify the presence and correct positioning of the
following parts:
a.
O-ring, MS28775-009
b.
Pin, Firing, P/N 8596416
c.
Retainer, Cartridge, P/N 10521325
d.
Cartridge, Impulse, M146, P/N 8596426
e.
Pin, Shear, P/N 8596419
f.
Piston, P/N 8596418
g.
Setscrew, P/N 10521326
h.
Spring, P/N 8596424
i.
Ring, Sealing (2 each), P/N 10520993
j.
Ring, Sealing, P/N 10520973
k.
Nut, Lock, P/N 10520981
l.
Head, P/N 10521324
m.
Cylinder, P/N 10521323
n.
Clevis, P/N 8596421
o.
Pin, Locking, P/N 8596422
p.
Setscrew, P/N 10543068-9
q.
Pin, Shear Unlock, P/N 8596423
r.
Packing, MS28775-001
s.
Piston, Floating, P/N 8596417
t.
Packing, MS28775-021
u.
Setscrew, P/N 10543068-1
v.
Plug, Protective, MIL-C-5501/10-F5
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
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