MIL-M-38510/22

Technical Characteristics

• End Item Identification

  helicopter, advance attack, ah-1w; helicopter, uscg search and rescue, hh-60j; helicopter, search and rescue, hh-60h; sturgeon class ssn (637); aircraft, c-2a (reprocured); helicopter, mh-53e; ticonderoga class cg (47); helicopter, carrier based asw,

• ~1

  data on certain environmental and performanc

• Specification/Standard Data

  81349-mil-m-38510/22 government specification

• Input Circuit Pattern

  dual 4 input

• Operating Temp Range

  -55.0/+125.0 deg celsius

• Voltage Rating And Type Per Characteristic

  -1.5 volts minimum power source and 5.5 volts maximum power source

• Criticality Code Justification

  feat

• Maximum Power Dissipation Rating

  296.0 milliwatts

• Features Provided

  hermetically sealed and w/enable and high speed and edge triggered and monolithic and positive outputs and w/clear

• Special Features

  weapon system essential

• Terminal Type And Quantity

  14 printed circuit

• Body Height

  0.140 inches minimum and 0.185 inches maximum

• Storage Temp Range

  -65.0/+150.0 deg celsius

• Design Function And Quantity

  2 flip-flop, j-k, clocked

• Body Width

  0.220 inches minimum and 0.310 inches maximum

• Terminal Surface Treatment

  solder

• Case Outline Source And Designator

  d-1 mil-m-38510

• Inclosure Material

  ceramic and glass

• Inclosure Configuration

  dual-in-line

• Body Length

  0.796 inches maximum

• Output Logic Form

  transistor-transistor logic

• ~1

  sh-60f; los angeles class ssn (688)

• 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