NSN 5962-01-168-0960
Part Details | LINEAR MICROCIRCUIT
5962-01-168-0960 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.
Alternate Parts: LH4640, PM356J, 6010467002, 6010467-002, JM3851011405BGB, JM38510/11405BGB, M3851011405BGX, M38510/11405BGX, M3851011405BGC, M38510/11405BGC, M3851011405BGA, M38510/11405BGA, MILM38510114, MIL-M-38510/114, 10129467, RB740T0, 9326271B, 932627-1B, 48430057, 4843-0057, 5962-01-168-0960, 01-168-0960, 5962011680960, 011680960
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | DEC 13, 1983 | 01-168-0960 | 31778 ( MICROCIRCUIT, LINEAR ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5962-01-168-0960
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| LH4640 | 34335 | ADVANCED MICRO DEVICES, INC.DBA A M D |
| PM356J | 06665 | ANALOG DEVICES, INC.DIV SANTA CLARA SITE |
| 6010467-002 | 12436 | BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION INC. |
| JM38510/11405BGB | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M38510/11405BGX | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M38510/11405BGC | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M38510/11405BGA | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-M-38510/114 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 10129467 | A486G | NIMIKKEISTOKESKUS NCB FINLAND |
| RB740T0 | 18324 | PHILIPS SEMICONDUCTORS INC |
| 932627-1B | 82577 | RAYTHEON COMPANYDBA RAYTHEON |
| 4843-0057 | 56269 | XKD CORPDBA DISPLAY SOLUTIONS |
Technical Data | NSN 5962-01-168-0960
| Characteristic | Specifications |
|---|---|
| DESIGN FUNCTION AND QUANTITY | 1 AMPLIFIER, OPERATIONAL, GENERAL PURPOSE |
| INPUT CIRCUIT PATTERN | 2 INPUT |
| VOLTAGE RATING AND TYPE PER CHARACTERISTIC | ACV20.0 VOLTS MAXIMUM |
| TIME RATING PER CHACTERISTIC | AEE100.00 NANOSECONDS MAXIMUM |
| OPERATING TEMP RANGE | -55.0 TO +125.0 DEG CELSIUS |
| TERMINAL TYPE AND QUANTITY | 8 PIN |
| TERMINAL SURFACE TREATMENT | SOLDER |
| INCLOSURE CONFIGURATION | CAN |
| INCLOSURE MATERIAL | METAL |
| CASE OUTLINE SOURCE AND DESIGNATOR | A-1 MIL-M-38510 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | JFET INPUT, WIDE BAND, LOW OFFSET |
| BODY OUTSIDE DIAMETER | 0.335 INCHES MINIMUM AND 0.370 INCHES MAXIMUM |
| BODY HEIGHT | 0.165 INCHES MINIMUM AND 0.185 INCHES MAXIMUM |
| MAXIMUM POWER DISSIPATION RATING | 330.0 MILLIWATTS |
| STORAGE TEMP RANGE | -65.0 TO +150.0 DEG CELSIUS |
| FEATURES PROVIDED | HERMETICALLY SEALED AND MONOLITHIC AND WIDEBAND AND W/FIELD EFFECT TRANSISTOR SWITCH |
| SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
| 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", "NOMINAL", ETC.). |
| SPECIFICATION/STANDARD DATA | 81349-MIL-M-38510 TO 114 GOVERNMENT SPECIFICATION |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | ENGINE, AIRCRAFT, F100 PW220 (F-15C/D/E); AIRCRAFT,(AC-130H, MC-130 |