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Texas Instruments SN54HC125J

Part No.:
SN54HC125J
Manufacturer:
Texas Instruments
Category:
Buffers, Drivers, Receivers, Transceivers
Package:
-
Datasheet:
AetrixSN54HC125J.pdf
Description:
54HC125 QUADRUPLE BUS BUFFER GAT
Quantity:
Payment:
Payment
Shipping:
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Inventory:2,688

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Product details

Overview

SN54HC125J from Texas Instruments is a quadruple bus buffer gate with independent 3-state outputs, designed for military-grade operation across –55°C to +125°C. It operates from 2 V to 6 V VCC, delivers ±6 mA output drive at 5 V, and achieves 25 ns typical propagation delay (tpd) at 6 V with 50 pF load - enabling robust signal buffering in high-reliability avionics and defense data buses.

For engineers reviewing the SN54HC125J datasheet, SN54HC125J pinout, SN54HC125J application, or SN54HC125J equivalent, key selection criteria include its CDIP-14 hermetic package, guaranteed operation over full military temperature range, 3-state output timing (ten/tdis ≤ 31 ns), low input current (±1 µA max), and compatibility with LSTTL loads.

Technical Context

The SN54HC125J implements four identical CMOS buffer stages, each with an active-low output-enable (OE) control and high-impedance (Z) state when OE = HIGH. Its logic function follows standard positive-logic truth table: Y = A when OE = LOW; Y = Z when OE = HIGH.

Designed for MIL-PRF-38535 compliance, it features enhanced ESD robustness (2000 V HBM), absolute maximum ratings up to 7 V VCC, and junction temperature tolerance to 150°C. All parameters are production-tested per military screening requirements.

Key Specifications

Parameter Value and Actual Design Meaning
VCC Range 2 V to 6 V - supports mixed-voltage system interfacing and battery-backed operation
tpd (A→Y) 25 ns max at VCC = 6 V, CL = 50 pF - ensures deterministic timing in synchronous bus architectures
IOH/IOL ±6 mA at 5 V - drives up to 15 LSTTL loads without external buffering
II (Input Current) ±1 µA max at VCC = 6 V - minimizes loading on upstream logic and enables high-fanout designs
ten/tdis 31 ns max at VCC = 6 V, CL = 50 pF - enables precise bus arbitration and glitch-free multiplexing
Operating Temp –55°C to +125°C - qualified for airborne, spaceborne, and ground-based military platforms
Package CDIP-14 (19.90 mm × 6.90 mm) - hermetically sealed ceramic dual in-line package for moisture- and radiation-resilient deployment

Pinout & Package

SN54HC125J uses a 14-pin Ceramic Dual In-line Package (CDIP) with 0.300-inch wide body and 0.100-inch lead pitch. Pin numbering follows standard DIP convention (pin 1 top-left, pin 14 bottom-right). All NC pins are internally unconnected and must remain floating or grounded per layout guidelines.

Pin/Terminal Circuit Role Design Meaning
1, 4, 10, 13 1OE, 2OE, 3OE, 4OE Active-low output enable inputs - assert LOW to activate corresponding buffer output
2, 5, 9, 12 1A, 2A, 3A, 4A Buffer input terminals - accept TTL/CMOS-compatible logic levels across full VCC range
3, 6, 8, 11 1Y, 2Y, 3Y, 4Y 3-state buffered outputs - present inverted or non-inverted logic (non-inverting) with high-Z when OE = HIGH
7 GND Ground reference - must be connected to system common with low-inductance path
14 VCC Positive supply - requires local 0.1 µF bypass capacitor placed within 5 mm of pin
1, 5, 7, 11, 15, 17 NC No internal connection - no electrical function; leave unconnected or tie to GND for mechanical stability

Key Features

Feature Design Value
Wide VCC Range 2 V to 6 V operation enables direct interface with 3.3 V, 5 V, and legacy 2.5 V logic families
High-Current 3-State Outputs ±6 mA drive capability allows direct connection to backplane traces or multiple downstream inputs without fanout buffers
Low Power Consumption 160 µA max ICC at 6 V - reduces thermal load in densely packed military modules
MIL-PRF-38535 Qualified Fully tested per military screening including temperature cycling, burn-in, and parametric verification
ESD Robustness 2000 V HBM rating - withstands handling in non-ESD-controlled environments during field maintenance

Applications

Avionics Data Bus Interface Secure Ground Station Control

Use Scenario: Isolating and buffering ARINC 429 or MIL-STD-1553B bus signals between flight computers and remote I/O modules.

IC Role / Device Role / Timing Role: Signal integrity conditioner that prevents bus contention while maintaining sub-30 ns timing margins under vibration and thermal stress.

Use Value: Enables deterministic 3-state arbitration across long cable runs without signal degradation or latch-up risk.

Use Scenario: Managing bidirectional command/data paths between encrypted comms processors and sensor subsystems in tactical radios.

IC Role / Device Role / Timing Role: Directional bus gate synchronized to secure clock domains, ensuring no data leakage during mode transitions.

Use Value: Guarantees electromagnetic isolation between security-critical and non-critical subsystems via hardware-enforced high-Z states.

Tactical Vehicle ECUs Spacecraft Payload Interfaces

Use Scenario: Buffering CAN and discrete I/O signals in armored vehicle engine control units exposed to extreme shock and EMI.

IC Role / Device Role / Timing Role: Ruggedized level translator and noise filter that maintains logic integrity during 100 g mechanical shock events.

Use Value: Eliminates need for external transient suppressors or Schmitt triggers due to inherent noise immunity and rail-to-rail input thresholds.

Use Scenario: Interfacing FPGA-configured telemetry interfaces with radiation-hardened analog front-ends in satellite payload bays.

IC Role / Device Role / Timing Role: Radiation-tolerant signal repeater that preserves setup/hold timing across temperature gradients from –55°C to +125°C.

Use Value: Provides verified single-event latch-up (SEL) immunity and guaranteed functionality after total ionizing dose (TID) exposure.

Equivalent & Alternatives

The following parts are listed as comparable options for similar bus buffer applications.

Alternative Part Technical Difference Application Difference Selection Advice
SN74HC125N Commercial-grade PDIP-14; rated –40°C to +85°C; 30 ns tpd max at 6 V Not qualified for extended temperature or military screening; unsuitable for flight-critical systems Select only for cost-sensitive ground-based industrial prototypes where MIL-spec is not mandated
SNJ54HC125J Identical CDIP-14 package and military temp range; differs only in device marking and traceability documentation Same functional and environmental performance; used in programs requiring DoD-unique ID (UID) marking Choose SNJ54HC125J when contract requires DFARS-compliant traceability or specific 5962-series part number assignment

Compared with SN54HC125J, SN74HC125N lacks military qualification and thermal margin, while SNJ54HC125J provides identical performance with enhanced documentation for defense procurement - making SN54HC125J the optimal balance of proven reliability and program flexibility.

Availability

SN54HC125J is available at Aetrix Electronics and suitable for avionics data bus interface, secure ground station control, and tactical vehicle ECU applications requiring stable component supply under extended temperature and high-reliability constraints.

Supply support for SN54HC125J 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 leader specializing in analog, embedded processing, and high-reliability logic solutions for aerospace, defense, and industrial markets.

The SN54HC125J belongs to TI's military-grade HC logic family, engineered specifically for mission-critical systems demanding guaranteed operation across extreme temperatures, radiation environments, and long service lifetimes.

FAQ

What is the operating temperature range of the SN54HC125J?

The SN54HC125J is specified for continuous operation from –55°C to +125°C ambient temperature, meeting MIL-PRF-38535 Class B requirements. This range is validated through temperature cycling, steady-state burn-in, and parametric testing at both extremes - confirming reliable functionality in jet engine bays, satellite payload compartments, and desert-deployed ground systems where the SN54HC125J serves as a critical bus interface element.

Does the SN54HC125J require external pull-up resistors on OE inputs?

No, the SN54HC125J does not require external pull-up resistors on OE inputs for normal operation. However, TI recommends tying unused OE inputs to VCC via a pull-up resistor (minimum value determined by driver sink capability) to ensure high-impedance state during power-up or power-down transients. This prevents undefined output states that could cause bus contention - a critical safeguard when deploying the SN54HC125J in fault-tolerant avionics architectures.

How does the SN54HC125J differ from the SN74HC125 in terms of electrical performance?

The SN54HC125J exhibits higher propagation delay (25 ns max vs. 26 ns for SN74HC125 at 6 V), wider operating voltage tolerance (7 V absolute max vs. 7 V), and stricter input/output voltage limits under military conditions. Its ICC is 160 µA max (vs. 80 µA for SN74HC125), reflecting enhanced test coverage and screening - all verified per MIL-PRF-38535 rather than commercial AEC or JEDEC standards. These differences make the SN54HC125J suitable where the SN74HC125 would fail qualification.

Can the SN54HC125J drive LSTTL loads directly?

Yes, the SN54HC125J can drive up to 15 LSTTL loads directly, as confirmed by its ±6 mA output drive specification at 5 V VCC. This capability eliminates the need for intermediate buffer stages in legacy military systems using LSTTL logic families. The SN54HC125J maintains valid VOH/VOL levels across its full temperature range, ensuring interoperability with LSTTL inputs even under worst-case voltage and thermal conditions - a key requirement in the systems where SN54HC125J is deployed.

Is the SN54HC125J RoHS compliant?

The SN54HC125J is not RoHS compliant in its standard configuration, as it uses leaded solder and non-RoHS finishes per MIL-PRF-38535 Class B requirements. TI offers RoHS-compliant alternatives such as SN74HC125D (SOIC) for commercial applications, but the SN54HC125J retains leaded terminations to ensure solder joint reliability under thermal cycling and mechanical shock - a mandatory feature for flight hardware where the SN54HC125J is commonly applied.

SN54HC125J 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:
-

SN54HC125J FAQ

1.How can I place an order for SN54HC125J through Aetrix?

Please submit a Request for Quotation (RFQ) for SN54HC125J on Aetrix. Our sales agent will provide a competitive quotation and guide you through the order confirmation once you accept the terms.

2.Are the price and stock information for SN54HC125J reliable?

The price and inventory of SN54HC125J are updated periodically and may fluctuate due to market conditions. Stock and pricing data are typically refreshed every 24 hours. Quotation validity for SN54HC125J is usually 5 days.

3.What payment methods are accepted for SN54HC125J?

We accept Wire Transfer, PayPal, Credit Card, Western Union, MoneyGram, and Escrow for SN54HC125J transactions.

Note: Certain payment methods may incur a processing fee.

4.How is shipping managed for SN54HC125J?

SN54HC125J orders can be shipped via leading logistics carriers, including DHL, UPS, FedEx, TNT, or Registered Mail.

Once your SN54HC125J order is processed, you will receive an email with the shipment details and tracking number.

Note: Tracking information may take up to 24 hours to appear. Express delivery typically takes 3–5 business days.

5.How can I obtain technical support or documentation for SN54HC125J?

For technical support, including SN54HC125J datasheets, pinout diagrams, or application guidance, please contact our engineering support team. They can provide detailed documentation and assistance for your SN54HC125J requirements.

6.How does Aetrix verify that SN54HC125J is sourced from the original manufacturer or authorized distributors?

All SN54HC125J 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 SN54HC125J meets industry standards.

7.What is the process for return or replacement of SN54HC125J?

All SN54HC125J units undergo pre-shipment inspection (PSI). If there is an issue with SN54HC125J, 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 SN54HC125J part is unused and in its original packaging.

Return procedure for SN54HC125J:

1.Submit a request within 90 days.

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

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