Downloaded from https://www.everyspec.com MIL-STD-81OD 19 JUIY ‘1983 FIGURES - Continued Ei.sMM 514.3-7 Basic transportation, composite taotical wheeled 514.3-8 environment, vertical axis Baaic transportation, composite tactical wheeled 514.3-13 environment, transverse axis Basio transportation, composite tactical wheeled 514.3-14 514.3-9 environment, longitudinal axia Basic transportation, tracked vehicle’(M548) 514.3-15 514.3-10 environment, vertical axis, test phase 1 Basic transportation, tracked vehicle (M548) 514.3-16 514.3-11 514.3-12 environment, vertical axis, test phase 2 Basic transportation, tracked vehicle (M548) 514.3-17 514.3-13 environment, vertical axia, test phase 3 Baaic transportation, tracked vehicle (M548) 514.3-18 environment, vertical axis, test phase 4 Basic transportation, tracked vehicle (M548) 514.3-19 514.3-14 environment, vertical axis, test phase 5 Basic transportation, tracked vehicle (M548) 514.3-20 514.3-15 environment, transverse axis, test phaae 1 Basic tranaportation, tracked vehicle (M548) 5,14.3-21 514.3-16 514.3-17 environment, transverse axis, test phase 2 Basic transportation, tracked vehicle “(M548) 514.3-22 514.3-18 environment, transverse axia, test phase 3 Basic transportation, tracked vehicle (M548) 514.3-23 environment, transverse axis, test phase Basic transportation, tracked vehicle (M548) 514.3-24 514.3-19 environment, longitudinal axia, teat phase 1 Basic transportation, tracked vehicle (M548) 514.3-25 514.3-20 environment, longitudinal axis, test phase 2 Basic tranaportation, tracked vehicle (M548) 514.3-26 514.3-21 514.3-22 environment, longitudinal axis, test phase 3 Basic transportation, tracked vehicle (M548) 514.3-27 514.3-23 514.3-24 514.3-25 environment, longitudinal axis, test phaae 4 Typical mission/field transportation scenario’ Typical package tester 514.3-28 51U.3-29 514.3-32 and equipment on engines Suggested vibration spectrum for jet aircraft equipment Reduction factor for mace loading Su~eated vibration spectrum for equipment mounted on helicopters Zones for rotary wing aircraft Response threshold spectrum for assembled external Suggested vibration spectra for propeller aircraft 514.3-36 514.3-39 514.3-39 514.3-26 514.3-27 514.3-28 514.3-29 514.3-30 514.3-41 514.3-42 stores carried on jet aircraft, in the absence of flight measurements Maneuver vibration response spectrum Dynamic pressure (q) as a function of Mach number 514.3-U9 514.3-49 514:3-31 514.3-32 514.3-33 514.3-50 Sugges~ed vibration test levels.for equipment installed- in external stores carried on jet aircraft 514.3-52 Threshold performance random vibration spectrum for and altitude 514.3-34 equipment installed in ships (non-combat) 514.3-55 Minimal integrity test - helicopters 514.3-56 514.3-35 viii