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Document ID:   MIL-STD-202       Scroll down to access document images
Spec/Std Sheet:  214

Overview
Title:  Method 214, Random Vibration
Scope:  This test is conducted for the purpose of determining the ability of component parts to withstand the dynamic stress exerted by random vibration applied between upper and lower frequency limits to simulate the vibration experienced in various service field environments. Random vibration is characteristic of modern field environments produced by missiles, high-thrust jets and rocket engines. In these types of environments, the random vibration provides a more realistic test. For design purposes, however, a swept frequency sinusoidal test may yield more pertinent design information.
Status:  Active Document Date:  24-OCT-2024      
  Next Review Due:  23-OCT-2029
59GP Doc Category:   Military Standard -Test Method Standard  

Responsibilities
Lead Standardization Activity:  CC  DLA Weapons Support (Columbus)  
  Preparing Activity: CC  DLA Weapons Support (Columbus)
Coordination:  Full  
Army Custodian:  CR   US Army Combat Capabilities Development Command, C5ISR Center  
Navy Custodian:  EC   Naval Information Warfare Systems Command  
Air Force Custodian:  85   Air Force Life Cycle Management Center - Electronic Components, Wire and Ca  
DLA Custodian:  CC   DLA Weapons Support (Columbus)  

Changes to military standards or handbooks issued after August 1, 2003 are incorporated in the modified document.
Revision History Click on column headings for a description of column content.
MediaDocument Part DescriptionDist StmtDocument DatePagesSize
Document ImageNotice 2 - ValidationA24-OCT-202412.0 KB
Document ImageNotice 1 - ValidationA22-JAN-202012.0 KB
Document ImageBase Document A18-APR-20159117.5 KB

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