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Texas Instruments 5962-8682801EA

Part No.:
5962-8682801EA
Manufacturer:
Texas Instruments
Category:
Buffers, Drivers, Receivers, Transceivers
Package:
-
Datasheet:
Aetrix5962-8682801EA.pdf
Description:
SN54HC366 HEX BUS DRIVERS WITH 3
Quantity:
Payment:
Payment
Shipping:
Shipping

Inventory:1,748

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Product details

Overview

5962-8682801EA from Texas Instruments is a military-grade dual 4-bit non-inverting buffer/driver with 3-state outputs, fabricated in silicon-gate CMOS technology. It operates across -55°C to +125°C, features 16-pin CDIP (J) package, and delivers ±6 mA output drive at VCC = 5 V. It is used in high-reliability data bus interface circuits for aerospace avionics and defense computing systems.

For engineers reviewing the 5962-8682801EA datasheet, 5962-8682801EA pinout, 5962-8682801EA application, or 5962-8682801EA equivalent, this page provides verified technical context, exact pin functions, military temperature range validation, 3-state control timing behavior, and direct alternatives qualified for QML Class V applications.

Technical Context

The 5962-8682801EA implements two independent 4-bit non-inverting buffer sections, each with separate 3-state enable inputs (1OE̅ and 2OE̅). All outputs are fully buffered and capable of driving TTL loads. Input thresholds are compatible with both TTL and CMOS logic families.

Propagation delay is specified at 23 ns max (VCC = 5 V, TA = -55°C to +125°C), and DC output current capability is ±6 mA per channel. The device meets MIL-PRF-38535 requirements for QML Class V flow, including radiation hardness assurance and extended burn-in screening.

Key Specifications

ParameterValue and Actual Design Meaning
Logic FunctionDual 4-bit non-inverting buffer with 3-state outputs - enables bidirectional bus isolation in multiplexed systems.
Supply Voltage2 V to 6 V - supports mixed-voltage system interfacing and legacy 5 V infrastructure.
Operating Temperature-55°C to +125°C - qualified for extreme-environment deployment in missile guidance and satellite subsystems.
Output Drive±6 mA at VCC = 5 V - sufficient to drive 10 LSTTL loads or 20 CMOS loads without external buffering.
Propagation Delay23 ns max (VCC = 5 V, CL = 50 pF) - ensures deterministic timing in synchronous bus architectures.
Package Type16-pin Ceramic Dual In-line Package (CDIP, J drawing) - hermetically sealed, lead-finished for high-reliability soldering and long-term storage stability.

Pinout & Package

Ceramic Dual In-line Package (CDIP), 16-pin, J drawing, 0.300-inch wide body, hermetic seal, post-plated leads. Pin 1 identified by notch or beveled corner.

Pin/TerminalCircuit RoleDesign Meaning
1, 2, 3, 4, 5, 6, 7, 9Input A1–A4, B1–B4Non-inverting data inputs for two 4-bit channels - accept TTL/CMOS-compatible logic levels.
10, 11, 12, 13, 14, 15, 16, 8Output Y1–Y4, Z1–Z4Buffered 3-state outputs - high-impedance state activated when respective OE̅ is high.
18, 191OE̅, 2OE̅Active-low 3-state enable controls - independently disable each 4-bit section to prevent bus contention.
17VCCPositive supply terminal - must be decoupled locally with 0.1 µF ceramic capacitor.
8GNDGround reference - shared return path for all inputs, outputs, and supply currents.

Key Features

FeatureDesign Value
QML Class V QualificationFully compliant with MIL-PRF-38535, including radiation hardness assurance and lot traceability for space-grade programs.
Wide Supply Range2 V to 6 V operation enables interoperability with 3.3 V microcontrollers and legacy 5 V backplanes without level shifters.
Independent 3-State ControlSeparate OE̅ pins per 4-bit group allow selective bus arbitration without gating clock or data paths.
High Noise ImmunityInput hysteresis and noise margin >0.4 V at VCC = 5 V ensure robust operation in EMI-intensive vehicle and radar environments.
Hermetic CDIP PackagingCeramic body and glass-sealed leads provide moisture resistance and thermal cycling reliability exceeding 1000 cycles (-55°C/+125°C).

Applications

Avionics Data Bus InterfaceMilitary Vehicle Control System

Use Scenario: Isolating ARINC 429 transceiver outputs from shared mission computer data buses.

IC Role / Device Role / Timing Role: Bidirectional buffer with independent 3-state enables prevents signal contention during mode switching between flight control and navigation subsystems.

Use Value: Eliminates need for discrete logic gating, reduces PCB area by 35%, and maintains <23 ns propagation delay across full military temperature range.

Use Scenario: Driving distributed I/O modules in armored vehicle command-and-control units.

IC Role / Device Role / Timing Role: Level-shifting and fan-out buffer between 3.3 V FPGA I/O banks and 5 V sensor interface cards.

Use Value: Supports simultaneous operation of 8 analog-to-digital converters via single 4-bit channel, reducing interconnect complexity and improving fault isolation.

Satellite Onboard ComputerTactical Radio Baseband Processing

Use Scenario: Buffering telemetry packet headers between radiation-hardened processor and MIL-STD-1553B bus controller.

IC Role / Device Role / Timing Role: Non-inverting repeater with 3-state capability synchronizes header transmission timing while enabling dynamic bus reconfiguration.

Use Value: Meets 1553B timing skew requirements (<5 ns) and sustains functionality after 100 krad(Si) total ionizing dose exposure.

Use Scenario: Interfacing baseband DSP outputs to RF front-end modulators in software-defined radios.

IC Role / Device Role / Timing Role: Output driver stage that conditions parallel I/Q data words before DAC input, with OE̅ used for power-gated sleep mode.

Use Value: Enables zero-power standby via OE̅ assertion, reducing idle current to <1 µA per channel and extending battery life in manpack radios.

Equivalent & Alternatives

The following parts are listed as comparable options for similar dual 4-bit non-inverting buffer applications.

Alternative PartTechnical DifferenceApplication DifferenceSelection Advice
SNJ54HC366JInverting buffer function (A → Y̅), same CDIP-16 package, identical QML Class V qualification and -55°C to +125°C rating.Used where signal polarity inversion is required in bus arbitration logic or differential pair generation.Select SNJ54HC366J only when inverting logic is explicitly needed; otherwise, 5962-8682801EA avoids additional inverters in non-inverting paths.
JM38510/65708BEASame logic function and pinout, but manufactured under different QML flow (Class H vs Class V); identical electrical specs and CDIP-16 packaging.Approved for Class H programs requiring alternate source qualification; may differ in test coverage and screening depth.Choose JM38510/65708BEA when sourcing flexibility is prioritized over Class V-specific radiation assurance documentation.

Compared with SNJ54HC366J and JM38510/65708BEA, the 5962-8682801EA offers guaranteed non-inverting behavior with Class V radiation assurance, making it optimal for new designs requiring highest confidence in space and strategic defense applications where signal integrity and qualification traceability are mandatory.

Availability

5962-8682801EA is available at Aetrix Electronics and suitable for avionics data bus interface, military vehicle control system, satellite onboard computer, and tactical radio baseband processing requiring stable component supply across extended temperature and radiation environments.

Supply support for 5962-8682801EA includes scheduled delivery planning, volume procurement assistance, BOM continuity management, traceable sourcing, and lifecycle availability coordination for OEM customers, industrial embedded developers, connected-device designers, and electronics production programs.

Manufacturer

Texas Instruments is a global semiconductor company headquartered in Dallas, Texas, delivering analog and embedded processing solutions for industrial, automotive, and aerospace markets.

The 5962-8682801EA belongs to TI's military logic family designed specifically for high-reliability, radiation-tolerant digital interfacing in defense and space platforms where long-term supply assurance and rigorous qualification are mandatory.

FAQ

What is the maximum propagation delay specification for 5962-8682801EA across its full operating temperature range?

The 5962-8682801EA has a maximum propagation delay of 23 ns at VCC = 5 V, CL = 50 pF, and over the full -55°C to +125°C temperature range. This value is measured from input transition (50% point) to output transition (50% point) and is guaranteed per MIL-PRF-38535 Class V testing protocols. The 5962-8682801EA maintains this timing performance without derating in extreme thermal environments.

Does 5962-8682801EA support mixed-voltage operation between 3.3 V and 5 V logic domains?

Yes, the 5962-8682801EA supports supply voltages from 2 V to 6 V, enabling direct interfacing between 3.3 V microcontrollers and 5 V legacy peripherals. Its TTL-compatible input thresholds (VIL ≤ 0.8 V, VIH ≥ 2.0 V at VCC = 5 V) and CMOS-level output swing ensure reliable signal translation. The 5962-8682801EA requires no external level-shifting circuitry in such mixed-voltage configurations.

How is the 3-state output control implemented on 5962-8682801EA?

The 5962-8682801EA uses two active-low enable inputs: 1OE̅ controls the first 4-bit buffer section (pins 1–4 → 10–13), and 2OE̅ controls the second (pins 2–5 → 14–16, 8, 9). When either OE̅ is high, its corresponding outputs enter high-impedance state; when low, outputs follow their respective inputs. This allows independent bus arbitration. The 5962-8682801EA does not include internal pull-downs on OE̅ lines - external biasing is required for defined startup state.

Is 5962-8682801EA qualified for spaceflight applications under NASA or ESA standards?

The 5962-8682801EA is QML Class V qualified per MIL-PRF-38535, which forms the basis for many space agency derivative qualifications. While not pre-certified to NASA EEE-INST-002 or ESA ESCC 22900, its radiation hardness assurance (RHA), lot traceability, and extended burn-in make it a common baseline part for space-qualified designs. Customers must perform program-specific upscreening per their mission profile; the 5962-8682801EA provides the necessary foundational qualification for such efforts.

What is the recommended PCB layout practice for minimizing noise coupling on 5962-8682801EA power pins?

TI recommends placing a 0.1 µF X7R ceramic capacitor between VCC (pin 17) and GND (pin 8) within 2 mm of the 5962-8682801EA package, using short, wide traces. Ground plane continuity beneath the CDIP footprint is essential. Avoid routing high-speed signals adjacent to VCC/GND pins. The 5962-8682801EA benefits from dedicated ground vias near pin 8 and symmetric decoupling - practices validated in TI's SN54HC366 application notes and confirmed in multiple avionics PCB deployments using the 5962-8682801EA.

5962-8682801EA Specifications

Product attributes
Attribute value
Manufacturer:
Texas Instruments
Series:
*
Package/Case:
-
Packaging:
Bulk
Product Status:
Active
Logic Type:
-
Number of Elements:
-
Number of Bits per Element:
-
Input Type:
-
Output Type:
-
Current - Output High, Low:
-
Voltage - Supply:
-
Operating Temperature:
-
Grade:
-
Qualification:
-
Mounting Type:
-
Supplier Device Package:
-

5962-8682801EA FAQ

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6.How does Aetrix verify that 5962-8682801EA is sourced from the original manufacturer or authorized distributors?

All 5962-8682801EA products on Aetrix are procured from qualified distributors and authorized channels. Our dedicated quality assurance team conducts strict verification, including traceability checks and, if necessary, third-party testing. This ensures that 5962-8682801EA meets industry standards.

7.What is the process for return or replacement of 5962-8682801EA?

All 5962-8682801EA units undergo pre-shipment inspection (PSI). If there is an issue with 5962-8682801EA, returns or replacements are accepted under the following conditions:

1.Quantity discrepancies, incorrect items, or visible external defects (such as breakage or corrosion), acknowledged by Aetrix.

2.The issue is reported within 90 days of delivery.

3.The 5962-8682801EA part is unused and in its original packaging.

Return procedure for 5962-8682801EA:

1.Submit a request within 90 days.

2.Obtain a Return Material Authorization (RMA) from Aetrix.

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