NSN 5962-01-046-9453
Part Details | LINEAR MICROCIRCUIT
5962-01-046-9453 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: 6010415001, 6010415-001, S8T09F883B, S8T09F/883B, RM8T09DC, 18201084, 1820-1084, S8T09F883B, S8T09F/883B, M385108T09BCB, M38510-8T09BCB, 900AS2007, 4806636402, 48-066364-02, 4806636402, 48-066364-02, 8T09BCA, 8T09/BCA, S8T09F883B, S8T09F/883B, N8T09F, 9516521, 951652-1, 9515721, 951572-1, RM8T09DC883B, RM8T09DC/883B, G3316035550, G331603-5550, 5962-01-046-9453, 01-046-9453, 5962010469453, 010469453
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | AUG 26, 1977 | 01-046-9453 | 31778 ( MICROCIRCUIT, LINEAR ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5962-01-046-9453
Part Number | Cage Code | Manufacturer |
---|---|---|
6010415-001 | 12436 | BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION INC. |
S8T09F/883B | 8V613 | BOEING COMPANY, THEDBA BOEING |
RM8T09DC | 07933 | FAIRCHILD SEMICONDUCTOR CORPSEMICONDUCTOR DIV HQ |
1820-1084 | 28480 | HEWLETT-PACKARD COMPANYDBA HP |
S8T09F/883B | 02731 | MCDONNELL DOUGLAS HELICOPTER CO INC |
M38510-8T09BCB | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
900AS2007 | 30003 | NAVAL AIR SYSTEMS COMMAND MANAGEDORIGINAL DESIGN ACTIVITY NOT |
48-066364-02 | 15280 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV ES DEFENSIVE SYSTEMS DIVISION |
48-066364-02 | 26916 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MULTIPLE |
8T09/BCA | 18324 | PHILIPS SEMICONDUCTORS INC |
S8T09F/883B | 18324 | PHILIPS SEMICONDUCTORS INC |
N8T09F | 18324 | PHILIPS SEMICONDUCTORS INC |
951652-1 | 49956 | RAYTHEON COMPANYDBA RAYTHEON |
951572-1 | 96214 | RAYTHEON COMPANYDBA RAYTHEON |
RM8T09DC/883B | 49956 | RAYTHEON COMPANYDBA RAYTHEON |
G331603-5550 | 49956 | RAYTHEON COMPANYDBA RAYTHEON |
Technical Data | NSN 5962-01-046-9453
Characteristic | Specifications |
---|---|
DESIGN FUNCTION AND QUANTITY | 4 DRIVER, BUS AND 4 DRIVER, LINE |
INPUT CIRCUIT PATTERN | QUAD 2 INPUT |
VOLTAGE RATING AND TYPE PER CHARACTERISTIC | ACV4.5 VOLTS MINIMUM AND ACV5.5 VOLTS MAXIMUM |
TIME RATING PER CHACTERISTIC | AEE20.00 NANOSECONDS MAXIMUM AND AED10.00 NANOSECONDS MAXIMUM |
OPERATING TEMP RANGE | -55.0 TO +125.0 DEG CELSIUS |
TERMINAL TYPE AND QUANTITY | 14 PRINTED CIRCUIT |
TERMINAL SURFACE TREATMENT | SOLDER |
INCLOSURE CONFIGURATION | DUAL-IN-LINE |
INCLOSURE MATERIAL | CERAMIC AND GLASS |
CASE OUTLINE SOURCE AND DESIGNATOR | D-1 MIL-M-38510 |
BODY LENGTH | 0.796 INCHES MAXIMUM |
BODY HEIGHT | 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM |
BODY WIDTH | 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM |
MAXIMUM POWER DISSIPATION RATING | 785.0 MILLIWATTS |
STORAGE TEMP RANGE | -65.0 TO +200.0 DEG CELSIUS |
FEATURES PROVIDED | HERMETICALLY SEALED AND POSITIVE OUTPUTS AND 3-STATE OUTPUT |
TEST DATA DOCUMENT | 96906-MIL-STD-883 STANDARD (INCLUDES INDUSTRY OR ASSOCIATION STANDARDS, INDIVIDUAL MANUFACTUREER STANDARDS, ETC.). |