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    DSA00191619.pdf by C-MAC Frequency Products

    • ISSUE 1; 19 JUNE 1998 n Shock: IEC 68-2-27 test Ea (MIL-STD-202 Method 213), ½ Sinewave 981m/s2 for 11ms, three shocks in each plane n Damp Heat: IEC 68-2-3 test Ca (steady state), durat
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