143A688-2

Technical Characteristics

• End Item Identification

  ac-130h, mc-130h, ec-130e, hc-130 aircraft. landing craft air cushion (lcac), f101-ge-102 engine (b-1) aircraft. communications systems an/wsc-3. interferometer diection finding system an/bld-1. tactical air opns module (an/tyq-(23). sh-60f asw

• Body Width

  0.245 inches minimum and 0.271 inches maximum

• Output Logic Form

  emitter-coupled logic

• Operating Temp Range

  -55.0/+125.0 deg celsius

• ~1

  carrier-based helicopter. sturgeon class ssn (637), los

• Criticality Code Justification

  feat

• Special Features

  weapon system essential

• Voltage Rating And Type Per Characteristic

  0.0 volts maximum power source

• Design Function And Quantity

  1 prescaler

• Body Length

  0.750 inches minimum and 0.785 inches maximum

• Input Circuit Pattern

  6 input

• Test Data Document

  96906-mil-std-883 standard (includes industry or association standards, individual manufactureer standards, etc.).

• 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

• Unpackaged Unit Weight

  2.0 grams

• Terminal Surface Treatment

  solder

• Features Provided

  monolithic and hermetically sealed and positive outputs

• Inclosure Material

  ceramic and glass

• Inclosure Configuration

  dual-in-line

• Maximum Power Dissipation Rating

  300.0 milliwatts