839184-0014

Technical Characteristics

• Test Data Document

  13973-839184 drawing (this is the basic governing drawing, such as a contractor drawing, original equipment manufacturer drawing, etc.; excludes any specification, standard or other document that may be referenced in a basic governing drawing)

• Body Height

  0.140 inches minimum and 0.185 inches maximum

• Terminal Type And Quantity

  16 printed circuit

• Storage Temp Range

  -65.0/+150.0 deg celsius

• Body Length

  0.840 inches maximum

• Body Width

  0.220 inches minimum and 0.310 inches maximum

• Inclosure Material

  ceramic

• Design Function And Quantity

  4 driver, line differential

• Terminal Surface Treatment

  solder

• Input Circuit Pattern

  5 input

• Maximum Power Dissipation Rating

  600.0 milliwatts

• Inclosure Configuration

  dual-in-line

• Voltage Rating And Type Per Characteristic

  15.0 volts maximum power source

• Output Logic Form

  transistor-transistor logic

• End Item Identification

  tactical air opns module (an/tyq-(23); aircraft, ac-130h, mc-130h, ec-130e, hc-130); recency net system (an/trc-179(v), an/frc-180(v), an/grc-215); helicopter, uscg search and rescue, hh-60j; helicopter, search and rescue, hh-60h; landing craft air

• Time Rating Per Chacteristic

  300.00 nanoseconds maximum propagation delay time, low to high level output and 300.00 nanoseconds maximum propagation delay time, high to low level output

• Features Provided

  hermetically sealed and w/enable and low power and schottky

• Operating Temp Range

  -55.0/+125.0 deg celsius

• Case Outline Source And Designator

  d-2 mil-m-38510

• Criticality Code Justification

  feat

• Special Features

  weapon system essential

• ~1

  cushion (lcac); communications systems an/wsc-3); c