Features and Characteristics
Body Width
Between 0.220 inches and 0.310 inches
Body Height
Between 0.140 inches and 0.185 inches
Maximum Power Dissipation Rating
400.0 milliwatts
Operating Tempurature Range
-55.0/+125.0 degrees celsius
Storage Tempurature Range
-65.0/+150.0 degrees celsius
End Application
Engine, aircraft tf33-pw-102 (c-135e, ec-135h/k/p); countermeasure set an/slq-32; trainer, b-1b aircraft; test station, oq-29 (v)msm; missile, tomahawk; support equipment, b-1 aircraft; support equipment, b-52 aircraft; missile, air-to-air, phoenix (aim-54) ; aircraft, ( ac-130h, mc-130h, ec-130e, h
Inclosure Material
Ceramic and glass
Inclosure Configuration
Dual-in-line
Input Circuit Pattern
Dual 5 input
Criticality Code Justification
Feat
Design Function And Quantity
2 receiver, line differential
Case Outline Source And Designator
D-2 mil-m-38510
Terminal Surface Treatment
Solder
Voltage Rating And Type Per Characteristic
-20.0 volts power source and 20.0 volts power source
Time Rating Per Chacteristic
75.00 nanoseconds propagation delay time, low to high level output and 75.00 nanoseconds propagation delay time, high to low level output
Special Features
Weapon system essential; design analysis
Nuclear Hardness Critical Feature
Hardened
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 data on certain environmental and performance requirements and test conditions that are shown as "typical", "average", "", etc.).
Terminal Type And Quantity
16 printed circuit
Specification Data
81349-mil-m-38510/104 government specification
FSC
5962 Electronic Microcircuits
NSN: 5962-00-584-3996
