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5962-00-584-3996
20 Products
000-3002-495
MICROCIRCUIT,LINEAR
NSN, MFG P/N
5962005843996
NSN
5962-00-584-3996
MFG
BOEING COMPANY THE DBA BOEING DIV DEFENSE SPACE & SECURITY - NETWORK & SPACE SYSTEMS
Description
BODY HEIGHT: 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM
BODY LENGTH: 0.896 INCHES MAXIMUM
BODY WIDTH: 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM
CASE OUTLINE SOURCE AND DESIGNATOR: D-2 MIL-M-38510
CRITICALITY CODE JUSTIFICATION: FEAT
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: M38510/10404BEA
DESIGN FUNCTION AND QUANTITY: 2 RECEIVER, LINE DIFFERENTIAL
III 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
INCLOSURE CONFIGURATION: DUAL-IN-LINE
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: DUAL 5 INPUT
MANUFACTURERS CODE: 81349
MAXIMUM POWER DISSIPATION RATING: 400.0 MILLIWATTS
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: MIL-M-38510/104
NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
Related Searches:
ROM/PROM FAMILY 001
MICROCIRCUIT,MEMORY
NSN, MFG P/N
5962005842285
NSN
5962-00-584-2285
ROM/PROM FAMILY 001
MICROCIRCUIT,MEMORY
NSN, MFG P/N
5962005842285
NSN
5962-00-584-2285
MFG
DLA LAND AND MARITIME
Description
(NON-CORE DATA) BIT QUANTITY: 512
(NON-CORE DATA) WORD QUANTITY: 64
BODY HEIGHT: 0.050 INCHES MINIMUM AND 0.085 INCHES MAXIMUM
BODY LENGTH: 0.370 INCHES MINIMUM AND 0.395 INCHES MAXIMUM
BODY WIDTH: 0.250 INCHES MINIMUM AND 0.260 INCHES MAXIMUM
DESIGN CONTROL REFERENCE: 932085-579B
FEATURES PROVIDED: HERMETICALLY SEALED AND MONOLITHIC AND POSITIVE OUTPUTS AND W/ENABLE AND EXPANDABLE AND W/BUFFERED OUTPUT AND WIRE-OR OUTPUTS AND BIPOLAR AND PROGRAMMABLE AND PROGRAMMED AND W/DECODED OUTPUT
III END ITEM IDENTIFICATION: TYPE F-TF-15A AIRCRAFT
INCLOSURE CONFIGURATION: FLAT PACK
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: 8 INPUT
MANUFACTURERS CODE: 82577
MAXIMUM POWER DISSIPATION RATING: 500.0 MILLIWATTS
MEMORY DEVICE TYPE: ROM
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
OUTPUT LOGIC FORM: TRANSISTOR-TRANSISTOR LOGIC
STORAGE TEMP RANGE: -65.0 TO 150.0 DEG CELSIUS
TERMINAL SURFACE TREATMENT: SOLDER
TERMINAL TYPE AND QUANTITY: 24 FLAT LEADS_!
Related Searches:
SCM780FH39
MICROCIRCUIT,MEMORY
NSN, MFG P/N
5962005842285
NSN
5962-00-584-2285
MFG
FREESCALE SEMICONDUCTOR INC.
Description
(NON-CORE DATA) BIT QUANTITY: 512
(NON-CORE DATA) WORD QUANTITY: 64
BODY HEIGHT: 0.050 INCHES MINIMUM AND 0.085 INCHES MAXIMUM
BODY LENGTH: 0.370 INCHES MINIMUM AND 0.395 INCHES MAXIMUM
BODY WIDTH: 0.250 INCHES MINIMUM AND 0.260 INCHES MAXIMUM
DESIGN CONTROL REFERENCE: 932085-579B
FEATURES PROVIDED: HERMETICALLY SEALED AND MONOLITHIC AND POSITIVE OUTPUTS AND W/ENABLE AND EXPANDABLE AND W/BUFFERED OUTPUT AND WIRE-OR OUTPUTS AND BIPOLAR AND PROGRAMMABLE AND PROGRAMMED AND W/DECODED OUTPUT
III END ITEM IDENTIFICATION: TYPE F-TF-15A AIRCRAFT
INCLOSURE CONFIGURATION: FLAT PACK
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: 8 INPUT
MANUFACTURERS CODE: 82577
MAXIMUM POWER DISSIPATION RATING: 500.0 MILLIWATTS
MEMORY DEVICE TYPE: ROM
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
OUTPUT LOGIC FORM: TRANSISTOR-TRANSISTOR LOGIC
STORAGE TEMP RANGE: -65.0 TO 150.0 DEG CELSIUS
TERMINAL SURFACE TREATMENT: SOLDER
TERMINAL TYPE AND QUANTITY: 24 FLAT LEADS_!
Related Searches:
000-8005-667
MICROCIRCUIT,LINEAR
NSN, MFG P/N
5962005843996
NSN
5962-00-584-3996
MFG
BOEING COMPANY THE DBA BOEING DIV DEFENSE SPACE & SECURITY - NETWORK & SPACE SYSTEMS
Description
BODY HEIGHT: 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM
BODY LENGTH: 0.896 INCHES MAXIMUM
BODY WIDTH: 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM
CASE OUTLINE SOURCE AND DESIGNATOR: D-2 MIL-M-38510
CRITICALITY CODE JUSTIFICATION: FEAT
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: M38510/10404BEA
DESIGN FUNCTION AND QUANTITY: 2 RECEIVER, LINE DIFFERENTIAL
III 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
INCLOSURE CONFIGURATION: DUAL-IN-LINE
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: DUAL 5 INPUT
MANUFACTURERS CODE: 81349
MAXIMUM POWER DISSIPATION RATING: 400.0 MILLIWATTS
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: MIL-M-38510/104
NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
Related Searches:
000-8007-646
MICROCIRCUIT,LINEAR
NSN, MFG P/N
5962005843996
NSN
5962-00-584-3996
MFG
BOEING COMPANY THE DBA BOEING DIV DEFENSE SPACE & SECURITY - NETWORK & SPACE SYSTEMS
Description
BODY HEIGHT: 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM
BODY LENGTH: 0.896 INCHES MAXIMUM
BODY WIDTH: 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM
CASE OUTLINE SOURCE AND DESIGNATOR: D-2 MIL-M-38510
CRITICALITY CODE JUSTIFICATION: FEAT
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: M38510/10404BEA
DESIGN FUNCTION AND QUANTITY: 2 RECEIVER, LINE DIFFERENTIAL
III 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
INCLOSURE CONFIGURATION: DUAL-IN-LINE
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: DUAL 5 INPUT
MANUFACTURERS CODE: 81349
MAXIMUM POWER DISSIPATION RATING: 400.0 MILLIWATTS
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: MIL-M-38510/104
NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
Related Searches:
103776-01
MICROCIRCUIT,LINEAR
NSN, MFG P/N
5962005843996
NSN
5962-00-584-3996
MFG
ROLM CORP MIL SPEC COMPUTERS
Description
BODY HEIGHT: 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM
BODY LENGTH: 0.896 INCHES MAXIMUM
BODY WIDTH: 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM
CASE OUTLINE SOURCE AND DESIGNATOR: D-2 MIL-M-38510
CRITICALITY CODE JUSTIFICATION: FEAT
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: M38510/10404BEA
DESIGN FUNCTION AND QUANTITY: 2 RECEIVER, LINE DIFFERENTIAL
III 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
INCLOSURE CONFIGURATION: DUAL-IN-LINE
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: DUAL 5 INPUT
MANUFACTURERS CODE: 81349
MAXIMUM POWER DISSIPATION RATING: 400.0 MILLIWATTS
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: MIL-M-38510/104
NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
Related Searches:
1063808-22
MICROCIRCUIT,LINEAR
NSN, MFG P/N
5962005843996
NSN
5962-00-584-3996
MFG
RAYTHEON COMPANY DBA RAYTHEON
Description
BODY HEIGHT: 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM
BODY LENGTH: 0.896 INCHES MAXIMUM
BODY WIDTH: 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM
CASE OUTLINE SOURCE AND DESIGNATOR: D-2 MIL-M-38510
CRITICALITY CODE JUSTIFICATION: FEAT
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: M38510/10404BEA
DESIGN FUNCTION AND QUANTITY: 2 RECEIVER, LINE DIFFERENTIAL
III 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
INCLOSURE CONFIGURATION: DUAL-IN-LINE
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: DUAL 5 INPUT
MANUFACTURERS CODE: 81349
MAXIMUM POWER DISSIPATION RATING: 400.0 MILLIWATTS
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: MIL-M-38510/104
NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
Related Searches:
118260-1073
MICROCIRCUIT,LINEAR
NSN, MFG P/N
5962005843996
NSN
5962-00-584-3996
MFG
NORTHROP GRUMMAN GUIDANCE AND ELECTRONICS COMPANY INC. DBA NAVIGATION SYSTEMS DIVISION DIV NAVIGATION SYSTEMS DIVISION
Description
BODY HEIGHT: 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM
BODY LENGTH: 0.896 INCHES MAXIMUM
BODY WIDTH: 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM
CASE OUTLINE SOURCE AND DESIGNATOR: D-2 MIL-M-38510
CRITICALITY CODE JUSTIFICATION: FEAT
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: M38510/10404BEA
DESIGN FUNCTION AND QUANTITY: 2 RECEIVER, LINE DIFFERENTIAL
III 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
INCLOSURE CONFIGURATION: DUAL-IN-LINE
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: DUAL 5 INPUT
MANUFACTURERS CODE: 81349
MAXIMUM POWER DISSIPATION RATING: 400.0 MILLIWATTS
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: MIL-M-38510/104
NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
Related Searches:
13081948-1
MICROCIRCUIT,LINEAR
NSN, MFG P/N
5962005843996
NSN
5962-00-584-3996
MFG
LOCKHEED MARTIN CORPORATION DBA LOCKHEED MARTIN
Description
BODY HEIGHT: 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM
BODY LENGTH: 0.896 INCHES MAXIMUM
BODY WIDTH: 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM
CASE OUTLINE SOURCE AND DESIGNATOR: D-2 MIL-M-38510
CRITICALITY CODE JUSTIFICATION: FEAT
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: M38510/10404BEA
DESIGN FUNCTION AND QUANTITY: 2 RECEIVER, LINE DIFFERENTIAL
III 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
INCLOSURE CONFIGURATION: DUAL-IN-LINE
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: DUAL 5 INPUT
MANUFACTURERS CODE: 81349
MAXIMUM POWER DISSIPATION RATING: 400.0 MILLIWATTS
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: MIL-M-38510/104
NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
Related Searches:
15384-001
MICROCIRCUIT,LINEAR
NSN, MFG P/N
5962005843996
NSN
5962-00-584-3996
MFG
ASTRONAUTICS CORPORATION OF AMERICA
Description
BODY HEIGHT: 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM
BODY LENGTH: 0.896 INCHES MAXIMUM
BODY WIDTH: 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM
CASE OUTLINE SOURCE AND DESIGNATOR: D-2 MIL-M-38510
CRITICALITY CODE JUSTIFICATION: FEAT
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: M38510/10404BEA
DESIGN FUNCTION AND QUANTITY: 2 RECEIVER, LINE DIFFERENTIAL
III 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
INCLOSURE CONFIGURATION: DUAL-IN-LINE
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: DUAL 5 INPUT
MANUFACTURERS CODE: 81349
MAXIMUM POWER DISSIPATION RATING: 400.0 MILLIWATTS
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: MIL-M-38510/104
NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
Related Searches:
158574-01
MICROCIRCUIT,LINEAR
NSN, MFG P/N
5962005843996
NSN
5962-00-584-3996
MFG
GE AVIATION SYSTEMS LLC
Description
BODY HEIGHT: 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM
BODY LENGTH: 0.896 INCHES MAXIMUM
BODY WIDTH: 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM
CASE OUTLINE SOURCE AND DESIGNATOR: D-2 MIL-M-38510
CRITICALITY CODE JUSTIFICATION: FEAT
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: M38510/10404BEA
DESIGN FUNCTION AND QUANTITY: 2 RECEIVER, LINE DIFFERENTIAL
III 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
INCLOSURE CONFIGURATION: DUAL-IN-LINE
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: DUAL 5 INPUT
MANUFACTURERS CODE: 81349
MAXIMUM POWER DISSIPATION RATING: 400.0 MILLIWATTS
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: MIL-M-38510/104
NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
Related Searches:
161883-405
MICROCIRCUIT,LINEAR
NSN, MFG P/N
5962005843996
NSN
5962-00-584-3996
MFG
BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION I
Description
BODY HEIGHT: 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM
BODY LENGTH: 0.896 INCHES MAXIMUM
BODY WIDTH: 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM
CASE OUTLINE SOURCE AND DESIGNATOR: D-2 MIL-M-38510
CRITICALITY CODE JUSTIFICATION: FEAT
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: M38510/10404BEA
DESIGN FUNCTION AND QUANTITY: 2 RECEIVER, LINE DIFFERENTIAL
III 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
INCLOSURE CONFIGURATION: DUAL-IN-LINE
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: DUAL 5 INPUT
MANUFACTURERS CODE: 81349
MAXIMUM POWER DISSIPATION RATING: 400.0 MILLIWATTS
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: MIL-M-38510/104
NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
Related Searches:
204-14935-2
MICROCIRCUIT,LINEAR
NSN, MFG P/N
5962005843996
NSN
5962-00-584-3996
MFG
THE BOEING COMPANY DBA BOEING
Description
BODY HEIGHT: 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM
BODY LENGTH: 0.896 INCHES MAXIMUM
BODY WIDTH: 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM
CASE OUTLINE SOURCE AND DESIGNATOR: D-2 MIL-M-38510
CRITICALITY CODE JUSTIFICATION: FEAT
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: M38510/10404BEA
DESIGN FUNCTION AND QUANTITY: 2 RECEIVER, LINE DIFFERENTIAL
III 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
INCLOSURE CONFIGURATION: DUAL-IN-LINE
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: DUAL 5 INPUT
MANUFACTURERS CODE: 81349
MAXIMUM POWER DISSIPATION RATING: 400.0 MILLIWATTS
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: MIL-M-38510/104
NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
Related Searches:
226630-000
MICROCIRCUIT,LINEAR
NSN, MFG P/N
5962005843996
NSN
5962-00-584-3996
MFG
BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION I
Description
BODY HEIGHT: 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM
BODY LENGTH: 0.896 INCHES MAXIMUM
BODY WIDTH: 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM
CASE OUTLINE SOURCE AND DESIGNATOR: D-2 MIL-M-38510
CRITICALITY CODE JUSTIFICATION: FEAT
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: M38510/10404BEA
DESIGN FUNCTION AND QUANTITY: 2 RECEIVER, LINE DIFFERENTIAL
III 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
INCLOSURE CONFIGURATION: DUAL-IN-LINE
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: DUAL 5 INPUT
MANUFACTURERS CODE: 81349
MAXIMUM POWER DISSIPATION RATING: 400.0 MILLIWATTS
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: MIL-M-38510/104
NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
Related Searches:
28627-40083
MICROCIRCUIT,LINEAR
NSN, MFG P/N
5962005843996
NSN
5962-00-584-3996
MFG
SELEX GALILEO LTD
Description
BODY HEIGHT: 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM
BODY LENGTH: 0.896 INCHES MAXIMUM
BODY WIDTH: 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM
CASE OUTLINE SOURCE AND DESIGNATOR: D-2 MIL-M-38510
CRITICALITY CODE JUSTIFICATION: FEAT
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: M38510/10404BEA
DESIGN FUNCTION AND QUANTITY: 2 RECEIVER, LINE DIFFERENTIAL
III 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
INCLOSURE CONFIGURATION: DUAL-IN-LINE
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: DUAL 5 INPUT
MANUFACTURERS CODE: 81349
MAXIMUM POWER DISSIPATION RATING: 400.0 MILLIWATTS
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: MIL-M-38510/104
NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
Related Searches:
3001-500
MICROCIRCUIT,LINEAR
NSN, MFG P/N
5962005843996
NSN
5962-00-584-3996
MFG
RAYTHEON COMPANY DBA RAYTHEON
Description
BODY HEIGHT: 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM
BODY LENGTH: 0.896 INCHES MAXIMUM
BODY WIDTH: 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM
CASE OUTLINE SOURCE AND DESIGNATOR: D-2 MIL-M-38510
CRITICALITY CODE JUSTIFICATION: FEAT
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: M38510/10404BEA
DESIGN FUNCTION AND QUANTITY: 2 RECEIVER, LINE DIFFERENTIAL
III 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
INCLOSURE CONFIGURATION: DUAL-IN-LINE
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: DUAL 5 INPUT
MANUFACTURERS CODE: 81349
MAXIMUM POWER DISSIPATION RATING: 400.0 MILLIWATTS
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: MIL-M-38510/104
NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
Related Searches:
349-113-061
MICROCIRCUIT,LINEAR
NSN, MFG P/N
5962005843996
NSN
5962-00-584-3996
MFG
INTERSTATE ELECTRONICS CORPORATION
Description
BODY HEIGHT: 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM
BODY LENGTH: 0.896 INCHES MAXIMUM
BODY WIDTH: 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM
CASE OUTLINE SOURCE AND DESIGNATOR: D-2 MIL-M-38510
CRITICALITY CODE JUSTIFICATION: FEAT
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: M38510/10404BEA
DESIGN FUNCTION AND QUANTITY: 2 RECEIVER, LINE DIFFERENTIAL
III 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
INCLOSURE CONFIGURATION: DUAL-IN-LINE
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: DUAL 5 INPUT
MANUFACTURERS CODE: 81349
MAXIMUM POWER DISSIPATION RATING: 400.0 MILLIWATTS
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: MIL-M-38510/104
NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
Related Searches:
351-1168-010
MICROCIRCUIT,LINEAR
NSN, MFG P/N
5962005843996
NSN
5962-00-584-3996
MFG
ROCKWELL COLLINS INC. DIV GOVERNMENT SYSTEMS - DALLAS
Description
BODY HEIGHT: 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM
BODY LENGTH: 0.896 INCHES MAXIMUM
BODY WIDTH: 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM
CASE OUTLINE SOURCE AND DESIGNATOR: D-2 MIL-M-38510
CRITICALITY CODE JUSTIFICATION: FEAT
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: M38510/10404BEA
DESIGN FUNCTION AND QUANTITY: 2 RECEIVER, LINE DIFFERENTIAL
III 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
INCLOSURE CONFIGURATION: DUAL-IN-LINE
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: DUAL 5 INPUT
MANUFACTURERS CODE: 81349
MAXIMUM POWER DISSIPATION RATING: 400.0 MILLIWATTS
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: MIL-M-38510/104
NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
Related Searches:
352250023743
MICROCIRCUIT,LINEAR
NSN, MFG P/N
5962005843996
NSN
5962-00-584-3996
MFG
THALES NEDERLAND
Description
BODY HEIGHT: 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM
BODY LENGTH: 0.896 INCHES MAXIMUM
BODY WIDTH: 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM
CASE OUTLINE SOURCE AND DESIGNATOR: D-2 MIL-M-38510
CRITICALITY CODE JUSTIFICATION: FEAT
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: M38510/10404BEA
DESIGN FUNCTION AND QUANTITY: 2 RECEIVER, LINE DIFFERENTIAL
III 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
INCLOSURE CONFIGURATION: DUAL-IN-LINE
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: DUAL 5 INPUT
MANUFACTURERS CODE: 81349
MAXIMUM POWER DISSIPATION RATING: 400.0 MILLIWATTS
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: MIL-M-38510/104
NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
Related Searches:
389352-1
MICROCIRCUIT,LINEAR
NSN, MFG P/N
5962005843996
NSN
5962-00-584-3996
MFG
EDO CORP DIV EDO CORPORATION ANTENNA PRODUCTS & TECHNOLOGIES
Description
BODY HEIGHT: 0.140 INCHES MINIMUM AND 0.185 INCHES MAXIMUM
BODY LENGTH: 0.896 INCHES MAXIMUM
BODY WIDTH: 0.220 INCHES MINIMUM AND 0.310 INCHES MAXIMUM
CASE OUTLINE SOURCE AND DESIGNATOR: D-2 MIL-M-38510
CRITICALITY CODE JUSTIFICATION: FEAT
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: M38510/10404BEA
DESIGN FUNCTION AND QUANTITY: 2 RECEIVER, LINE DIFFERENTIAL
III 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
INCLOSURE CONFIGURATION: DUAL-IN-LINE
INCLOSURE MATERIAL: CERAMIC AND GLASS
INPUT CIRCUIT PATTERN: DUAL 5 INPUT
MANUFACTURERS CODE: 81349
MAXIMUM POWER DISSIPATION RATING: 400.0 MILLIWATTS
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE: MIL-M-38510/104
NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED
OPERATING TEMP RANGE: -55.0 TO 125.0 DEG CELSIUS
