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MIL-S-48461B(AR)
TABLE VI. Test equipment.
Nomenclature
Part Number
Item
T e s t Set - Immersion Leak, Purge and Fill
1
11821748
T e s t Station, Sensor - Cant Angle
11822614
2
S e t t l i n g Time - Test Fixture
3
11823470
F i x t u r e - Vibration/Shock
4
11823471
Fixture - Altitude, Test Station
11823472
5
4.6.2 Performance tests.
4 . 6 . 2 . 1  Rotor output voltages. Use items 2 and 3 of table VI to verify
c o m p l i a n c e with the requirements of 3.3.1.
4 . 6 . 2 . 2 S t a t o r o u t p u t v o l t a g e s .  U s e items 2 and 3 of table VI to verify
c o m p l i a n c e with the requirements of 3.3.2.
4.6.2.3 Rotor voltages at null. Use items 2 and 3 of table VI to verify
c o m p l i a n c e with the requirements of 3.3.3.
4 . 6 . 2 . 4 Spurious signal components. Use items 2 and 3 of table VI to
v e r i f y compliance with the requirements of 3.3.4.
4.6.2.5 Settling time. Use items 2 and 3 of table VI to verify
c o m p l i a n c e with the requirements of 3.3.5.
4.6.3
Environmental
tests.
4.6.3.1 Shock.
4 . 6 . 3 . 1 . 1 B a s i c d e s i g n .  U s e item 4 of table VI and subject the assembly
t o the shock test specified in MIL-STD-810, method 516.2, procedure I, figure
5 1 5 . 2 - 2 . Apply three half sine wave shock pulses in each direction along the
t h r e e axes. Peak amplitude shall be 40 4 g with a time duration of 18 + 3
m s e c measured at the 10 percent amplitude points. At the conclusion of this
test, subject the assembly to the performance tests of 4.6.2.
16

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