‘,.,:. t..’ MlL–STD-s loB Downloaded from https://www.everyspec.com 15 June 1967 \ ~A R- 0.85 A TOLESANCELIUITS - / 1.15 A W / \ -;? g : ~ s ~~ S 1 SS J ?AV E T R A N S L A T E D / , DO W J W P J I 0.15 A l . \u // I D E A L S I N E W AV S __ J : \ ~ L _ \ ~ .2 A O ; : 3 Q Z H J i \ RB F L I N E Z E R G 0.05 A - ~ . 7 / - 0.2 A - 0.2 A L I PEAK vALi (A) k’ot.tTNAL DuRATION (D) MS \ 30CEOURE TEST FLIGHT VEHICLE EQUIPMENT (a) GROUND FLIGHT VEHICLE GROUND EQUIR.5N’I(b) SQUIPMZWT (c) EQUIFWZNT (d)/ I BASIC DESIGN 15 III CRASH Lmw’IT 30 IV HIGH INTENSITi 100 ITS: SHOCK PAF.AMtmERs(t ti -DBD FOR EQUIPMENT SHOCK MOUNTEC OR WEIGHIN 300 POUNDSOR MOP.S. Am (c):
FG3c .1 THE OSCILLIXXAM SRALL INCLUDE A TIME ABOUT 3D LONG WITH A PULSE I.QCATSDAPPROXIMATELY iIJ THE C3WTEF. TfE ACCELSBATION AMPLITUDE OF THE ID2,ALSALT SINE PULSE IS A AND ITS DUSATJO# IS D. ANY MEASURED ACCELESA’FIONPULSE WSICH CAN BE CONTAINED B2TWEEH THE BROKEN LINT BO~AS12S IS ACCEPTABLE. THE MEABUBJiDV31LDCITYCHANGE (i’UICHMAY BE OBTAINFD BY INTEGRA- TION OF TICSACCELERATION PULSE) SHALL BE WITHIN THX L13.UTSVi *O.1 Vi -E Vi IS THE V2Z.OCITY-CHANGEASSOCIATED WITS THE IDFAL PULSE WRICH lQUALS 2 AD/ti. THE INTBGP.ATIOX TO DETERhTNE VELOCITY CHANGE SHALL EXTESD FROM O.~D BEFOB2 THE POISE TO O.lD BSYOND TKE PULSE. ,,!. I FIGURZ516–2.
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