86121

Technical Characteristics

• ~1

  data on certain environmental and performanc

• Test Data Document

  81349-mil-m-38510 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

• End Item Identification

  aircraft, hornet f/a-18; aircraft, f-16; aircraft, airlifter c-17a; wasp class lhd; aircraft, galaxy c-5; f414 engine (f/a-18 f & g aircraft); aircraft, starlifter c-141

• Maximum Power Dissipation Rating

  200.0 milliwatts

• Storage Temp Range

  -65.0/+175.0 deg celsius

• Operating Temp Range

  -55.0/+125.0 deg celsius

• Body Width

  0.245 inches minimum and 0.285 inches maximum

• Inclosure Configuration

  flat pack

• Criticality Code Justification

  feat

• Voltage Rating And Type Per Characteristic

  15.5 volts maximum power source

• Special Features

  weapon system essential

• Output Logic Form

  complementary-metal oxide-semiconductor logic

• Design Function And Quantity

  6 buffer, inverting

• Terminal Surface Treatment

  solder

• Features Provided

  positive outputs and monolithic and hermetically sealed and true/complementary

• Body Length

  0.440 inches maximum

• Specification/standard Data

  81349-mil-m-38510/55 government specification

• Inclosure Material

  ceramic and glass

• Input Circuit Pattern

  hex 1 input

• Terminal Type And Quantity

  16 flat leads

• Time Rating Per Chacteristic

  345.00 nanoseconds maximum propagation delay time, low to high level output and 225.00 nanoseconds maximum propagation delay time, high to low level output

• Body Height

  0.045 inches minimum and 0.085 inches maximum

• Case Outline Source And Designator

  f-5 mil-m-38510