538292-2

Technical Characteristics

• ~1

  (an/tsc-93a), engine, aircraft tf33-pw-102 (c-135e, ec

• Dc Resistance Rating In Ohms

  0.220 single component single winding

• Criticality Code Justification

  feat

• Core Construction

  s0lid single component

• Special Features

  weapon system essential

• Inclosure Type

  fully inclosed

• Quality Factor

  28 minimum single component single winding

• Inductance Rating

  1.50 microhenries nominal single component single winding

• Maximum Operating Temp

  105.0 deg celsius

• Body Length

  0.240 inches minimum and 0.260 inches maximum

• Terminal Type And Quantity

  2 wire lead

• Reliability Indicator

  not established

• Overall Diameter

  0.085 inches minimum and 0.105 inches maximum

• Coil Form Type

  solid single component

• Rating Method

  electrical single component single winding

• Mounting Method

  terminal single group

• Winding Conductor Size

  0.02010 inches american wire gage single component single winding

• Winding Operating Current

  535.0 milliamperes maximum of standard range b and better drop siding single component single winding

• Specification/Standard Data

  96906-ms75084 government standard

• Test Data Document

  81349-mil-c-15305 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

• ~1

  data on certain environmental and performanc

• End Item Identification

  aircraft, sof ( ac-130h, mc-130h, ec-130e, hc-130), communications terminal, satellite an/gsc-39(v)1, ground mobile force satellite comm term (an/tsc-85a), missile, all-weather anti-ship, harpoon (agm-84), ground mobile force satellite comm term