. ,., , MIL-STD-8108 .; 15 June 1967 Downloaded from https://www.everyspec.com IDF.ALSAW’MOTB PULSE I%ERANCE LINITS / 0.15 P / P 0.05 P BXF LINE . . I ./ -0.15 P II -0.’2 P “T05P 1= + FLIGHTVEHICLE GROUND F L I G H T v F J II C L E G R O UN D PROCEOURI TEST EQUIPMENT (a) EQUIFMENT (b) EQuIPMENT (C) E Q U I F l @ N T ( d ) .PPAK VALUi. (P) NoMINAL DURA~on (D? ~j (‘Yt ...: I B A S I C D E S I G li 20 L ! o 11 18 III CR A S H S A F ~ 40 75 11 11 I V HIGH INTENSITY 100 100 6 11 m O T E : SHOCK PARAMETERS (a) AND (C): BXCO!.O.EliDEo FOR EQUIPMENT NOT SHOCK MOWED A N D WEIGSING LESS THAI 300 POUNIS.
T S E 0SCILIJYXL4M S H A LL I N C L U D E A T I M E A S O U T 3 D U X G w T S A P ~ S E ~ C A T E D A F ~ O X ~~ L y I N T H E C E N T E S . T H E P E A K A CC E L E R A T I O N MAGNITUDE OF THE SAhTOOTH PULSE IS P AND ITS DURATION IS D. ANY )+F.ASUBELOACCELERATION PUIi3EWHICH CAN BE CONTAINRD BETWEEN T~ BRO~ LINS BoUNDARIES IS ACCEPTABLE. THE MSASUNED VEIDCITY CSANGE (WHICH MAY BE OBTAINED BY INTF.G - TION OF THE ACCELERATION PULSE) SHALL BE WITHIN THE LIKi?TSOF vi M-l vi, -E U .’IS 2s VELOCITY CHANGE ASSOCIATES WITS THE IDEAL PUWE wSICS SQUALS 0.5 DP. ~ INTEG~T N ~ .DETEWNE VELGCCTY CHANGE SHALL EXTEND FROM 0.~D BEFORE TSE PULSE ‘IOO.m B~oNo TirE PULSE, FIGURE 516-1.
Termimzl.peak sawtooth chock pulse con,6guration and its tole.an.e limits. hlFWfIOD 516 516-6 r -----