Part Number
Part Number:
NSN:
NIIN:
Item Name:
MICROCIRCUIT , LINEAR
Definition:
A MICROCIRCUIT WHOSE OUTPUT IS A FUNCTION OF THE INPUT; THAT IS, THE OUTPUT VARIES IN A PREDETERMINED AND ESSENTIALLY PREDICTABLE MANNER FROM THE INPUT SIGNAL.
CAGE Information
| Code | Company |
|---|---|
| 49956 | RAYTHEON COMPANY DBA RAYTHEON |
Federal Supply Class
Title
MICROCIRCUITS, ELECTRONIC
Inclusions:
INCLUDES INTEGRATED CIRCUIT DEVICES; INTEGRATED CIRCUIT MODULES, INTEGRATED ELECTRONIC DEVICES: HYBRID, MAGNETIC, MOLECULAR, OPTO-ELECTRONIC, AND THIN FILM.
Exclusions:
EXCLUDES SINGLE CIRCUIT ELEMENTS SUCH AS CAPACITORS; RESISTORS; DIODES AND TRANSISTORS; PRINTED CIRCUIT BOARDS AND CIRCUIT CARD ASSEMBLIES; AND FILTERS AND NETWORKS.
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| CQSZ | INCLOSURE CONFIGURATION | DUAL-IN-LINE |
| AFGA | OPERATING TEMP RANGE | -55.0/+125.0 DEG CELSIUS |
| CQZP | INPUT CIRCUIT PATTERN | DUAL 5 INPUT |
| TEST | 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 |
| NHCF | NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |
| CZEN | VOLTAGE RATING AND TYPE PER CHARACTERISTIC | -20.0 VOLTS MINIMUM POWER SOURCE AND 20.0 VOLTS MAXIMUM POWER SOURCE |
| CZEQ | TIME RATING PER CHACTERISTIC | 75.00 NANOSECONDS MAXIMUM PROPAGATION DELAY TIME, LOW TO HIGH LEVEL OUTPUT AND 75.00 NANOSECONDS MAXIMUM PROPAGATION DELAY TIME, HIGH TO LOW LEVEL OUTPUT |
| AFJQ | STORAGE TEMP RANGE | -65.0/+150.0 DEG CELSIUS |
| ADAU | BODY HEIGHT | 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); COUNTERMEASURE SET AN/SLQ-32; TRAINER, B-1B AIRCRAFT; TEST STATION, OQ-290(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 |
| AEHX | MAXIMUM POWER DISSIPATION RATING | 400.0 MILLIWATTS |
| TTQY | TERMINAL TYPE AND QUANTITY | 16 PRINTED CIRCUIT |
| CQSJ | INCLOSURE MATERIAL | CERAMIC AND GLASS |
| ADAT | BODY WIDTH | 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM |
| ADAQ | BODY LENGTH | 0.896 INCHES MAXIMUM |
| CTFT | CASE OUTLINE SOURCE AND DESIGNATOR | D-2 MIL-M-38510 |
| ZZZK | SPECIFICATION/STANDARD DATA | 81349-MIL-M-38510/104 GOVERNMENT SPECIFICATION |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| FEAT | SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL; DESIGN ANALYSIS |
| CSSL | DESIGN FUNCTION AND QUANTITY | 2 RECEIVER, LINE DIFFERENTIAL |
| CWSG | TERMINAL SURFACE TREATMENT | SOLDER |