MIL-C-39010/1

Technical Characteristics

• ~1

  data on certain environmental and performanc

• Frequency At Which Inductance And Quality Factor Applies (Non-Core)

  25.0 megahertz single component single winding

• Core Construction

  s0lid single component

• Inclosure Type

  fully inclosed

• Quality Factor

  40 minimum single component single winding

• Reliability Indicator

  established

• Maximum Operating Temp

  105.0 deg celsius

• Special Features

  magnetically shielded; weapon system essential

• Dc Resistance Rating In Ohms

  0.590 single component single winding

• Overall Diameter

  0.152 inches minimum and 0.172 inches maximum

• Terminal Type And Quantity

  2 wire lead

• Reliability Failure Rate Level In Percent

  0.010

• Coil Form Type

  solid single component

• Test Data Document

  81349-mil-c-39010 specification (includes engineering type bulletins, brochures,etc., that reflect specification type data in specification format; excludes commercial catalogs, industry directories, and similar trade publications, reflecting general type

• Unpackaged Unit Weight (Non-Core)

  0.85 grams

• Criticality Code Justification

  feat

• Rating Method

  electrical single component single winding

• Mounting Method

  terminal single group

• End Item Identification

  helicopter, seahawk, h-60; helicopter, carrier based asw, sh-60f; spruance class dd (963); milstar system; kidd class ddg; patriot missile; f/a-18 hornet; lamps mark iii, sh-60b helicopter

• Inductance Rating

  0.82 microhenries nominal single component single winding

• Body Length

  0.390 inches minimum and 0.430 inches maximum

• Specification/Standard Data

  81349-mil-c-39010/1 government specification

• Minimum Self-Resonant Frequency (Non-Core)

  180.0 megahertz single component

• Winding Operating Current

  370.0 milliamperes maximum of standard range b single component single winding