MIL-T-46591B
numbers shall be in consecutive order beginning with the number 001 in each production lot. Any missing numbers are to be identified on the X-rays. The thrusters shall be arranged on trays or boards in consecutive numerical order, and each radiograph shall carry a permanent identification of the units displayed thereon. The radiographic plate identification shall include item nomenclature, the complete lot number, the span of serial numbers displayed, and the contract number. The radiographs of the entire production lot shall accompany the ballistic sample to the activity conducting the production lot acceptance test. Defective thrusters found during X-ray review are to be marked on the X-ray prior 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. Cartridge, Impulse M94, PIN 8596708 b. Setscrew, PIN MS51029-111
c. Pin, Shear, PIN 8593876 d. Pin, Firing, PIN 8593878 e. 0-ring, PIN AN6227-B7
f. Firing Pin Housing Assembly, PIN 10520880 g. 0-rings (two), PIN MS29513-122
h. Piston, Gas, PIN 10520887 i. 0-ring, PIN AN6227-B13
J. Pin, Unlock, Shear, PIN 10520882 k. 0-ring, PIN AN6227-B20
l. 0-ring, PIN AN6227-B13
m. Ring Nut Assembly, PIN 10520881 n. Ring Retaining, PIN 10520883
o. Spacer, Piston, PIN 10520888
p. Retainer (four), PIN MS35803-115 q. Reservoir Assembly, PIN 10520890
r. Piston Rod Assembly, PIN 10520885 s. Body, PIN 10520889
t. Rod, End, PIN 10520884 u. Gasket, PIN 10520878
v. Plug, PIN 10520879
w. Screw, Hollow Lock, PIN 10520900 x. 0-ring, PIN AN6227-B6
y. Spacer, Reservoir, PIN 10520886
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.
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