STMicroelectronics RHFACT14K1
- Part No.:
- RHFACT14K1
- Manufacturer:
- STMicroelectronics
- Category:
- Gates and Inverters
- Package:
- 14-CFlatPack
- Datasheet:
-
RHFACT14K1.pdf
- Description:
- RAD-HARD HEX SCHMITT INVERTER
- Quantity:
- Payment:

- Shipping:

Inventory:3,315
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Product details
Overview
RHFACT14K1 from STMicroelectronics is a radiation-hardened, high-speed CMOS logic device in the 54ACTxxx series - specifically a quad 2-input NAND gate - designed for aerospace and space-grade digital control systems. It operates at 4.5 V to 5.5 V, delivers TID hardness up to 300 krad(Si), exhibits SEL immunity up to 125 MeV·cm²/mg, and functions across –55 °C to +125 °C in hermetic ceramic Flat-14 packaging.
For engineers reviewing the RHFACT14K1 datasheet, RHFACT14K1 pinout, RHFACT14K1 application, or RHFACT14K1 equivalent, this part supports critical timing, combinatorial logic, and bus interface functions in radiation-intensive environments where latch-up immunity, single-event upset resilience, and guaranteed parametric performance at extreme temperature are mandatory selection criteria.
Technical Context
The RHFACT14K1 implements TTL-compatible input thresholds and CMOS output drive within a QML-V qualified rad-hard process. Its logic structure consists of four independent 2-input NAND gates with buffered outputs, each featuring Schmitt-trigger noise immunity on inputs per AC/ACT family design.
It uses ST's AMK6 6-inch diffusion line silicon, qualified under MIL-STD-883 cond A for total ionizing dose, and characterized against heavy-ion SEE using the 54AC14 test vehicle (Class 1: basic gates & Schmitt triggers), confirming SEL immunity and SEU/SET thresholds at 3 V and 4.5 V operating points.
Key Specifications
| Parameter | Value and Actual Design Meaning |
|---|---|
| VCC Range | 4.5 V to 5.5 V - ensures compatibility with standard 5 V TTL logic rails while maintaining radiation-hardened operation margins. |
| TID RHA | 300 krad(Si) - guaranteed functional survival under cumulative gamma/x-ray exposure typical of low-Earth orbit missions. |
| SEL Threshold | ≥125 MeV·cm²/mg - prevents destructive single-event latch-up during proton/heavy-ion bombardment in space. |
| Operating Temp | –55 °C to +125 °C - enables deployment in unheated satellite bays and deep-space probe electronics without thermal derating. |
| Package | Ceramic Flat-14 - hermetically sealed, lead-free, QML-V qualified package with grounded metallic lid for EMI suppression and thermal conduction. |
| Input Logic Type | TTL-compatible - accepts standard 5 V TTL input voltage levels (VIH ≥ 2.0 V, VIL ≤ 0.8 V), simplifying integration with legacy spacecraft buses. |
| Output Drive | CMOS - provides rail-to-rail swing (VOH ≥ VCC – 0.1 V, VOL ≤ 0.1 V) and symmetrical ±24 mA drive capability at VCC = 5 V. |
Pinout & Package
Ceramic Flat-14 package: 14-terminal surface-mount hermetic package with grounded metallic lid, 1.27 mm pitch, 9.27 mm × 6.19 mm footprint, and 2.72 mm max height. Lid electrically connected to Pin 7 (GND).
| Pin/Terminal | Circuit Role | Design Meaning |
|---|---|---|
| 1, 2, 4, 5, 8, 9, 11, 12 | Input (A/B per gate) | Dedicated logic inputs for four independent NAND gates; TTL-compatible thresholds ensure robust noise margin in noisy spacecraft harnesses. |
| 3, 6, 10, 13 | Output (Y per gate) | CMOS push-pull outputs capable of driving 50 pF loads with <10 ns propagation delay at VCC = 5 V and 25 °C. |
| 7 | GND | Primary ground reference and electrical connection point for hermetic lid - mandatory for EMI shielding and thermal path integrity. |
| 14 | VCC | Single positive supply input; must be decoupled locally with ≥100 nF ceramic capacitor to suppress switching transients in rad-hard systems. |
Key Features
| Feature | Design Value |
|---|---|
| QML-V qualification | Qualified per MIL-PRF-38535 Class V, enabling use in DoD and NASA flight programs without requalification. |
| SEL immunity | Immune to destructive latch-up up to 125 MeV·cm²/mg LET - eliminates need for external current-limiting or watchdog circuitry in high-radiation orbits. |
| Hermetic ceramic package | Zero moisture ingress and zero outgassing - meets NASA ASTM E595 requirements for vacuum stability in deep-space applications. |
| Rad-tolerant process | Manufactured on ST's AMK6 rad-hard process with oxide thickness and doping optimized to suppress charge trapping and interface state generation. |
| Wide temp range support | Guaranteed AC/DC parameters over –55 °C to +125 °C - avoids derating or thermal management overhead in thermally constrained payloads. |
Applications
| Onboard Command Decoder | Satellite Telemetry Formatter |
|---|---|
|
Use Scenario: Decoding discrete command pulses from S-band uplink receivers into enable signals for payload actuators and subsystem resets. IC Role / Device Role / Timing Role: Combinatorial logic gate implementing NAND-based address decoding and pulse synchronization with spacecraft master clock. Use Value: Eliminates need for redundant FPGA logic; provides deterministic, radiation-immune decode function with sub-10 ns propagation delay stability across temperature and dose. |
Use Scenario: Formatting raw sensor data streams from star trackers and gyros into standardized CCSDS telemetry frames before downlink transmission. IC Role / Device Role / Timing Role: Glue logic for bus arbitration, parity generation, and frame synchronization control in telemetry processing chains. Use Value: Enables deterministic timing alignment between analog front-end sampling and digital packetization, unaffected by TID accumulation up to end-of-mission dose. |
| Launch Vehicle Avionics Sequencer | Deep-Space Probe Power Controller |
|
Use Scenario: Implementing hardwired interlock logic for stage separation, fairing jettison, and engine ignition sequencing under high-vibration, high-radiation launch conditions. IC Role / Device Role / Timing Role: Radiation-immune combinational logic block generating time-critical enable/disable signals synchronized to inertial measurement unit triggers. Use Value: Guarantees fail-safe sequencing behavior without software intervention - critical for mission success when FPGA configuration memory may suffer SEUs. |
Use Scenario: Controlling isolated DC-DC converter enable lines and battery charge/discharge paths in Europa Clipper-class probes exposed to Jupiter's magnetospheric radiation belts. IC Role / Device Role / Timing Role: High-reliability level-shifting and signal conditioning interface between microcontroller GPIOs and power MOSFET gate drivers. Use Value: Maintains functional integrity after 300 krad(Si) exposure - avoids single-point failure in primary power distribution architecture. |
Equivalent & Alternatives
The following parts are listed as comparable options for similar quad 2-input NAND gate applications.
| Alternative Part | Technical Difference | Application Difference | Selection Advice |
|---|---|---|---|
| 54ACT00 (generic SMD) | Same logic function and radiation specs, but non-QML-V commercial-grade variant; lacks flight-qualified screening and lot traceability. | Acceptable for ground-test hardware or non-flight prototypes; not approved for flight use per NASA-SSP-30238 or ECSS-Q-ST-60C. | Select only for development or qualification test benches where full QML-V pedigree is not required. |
| RHFAC00 (STMicroelectronics) | AC-series variant: lower VCC range (2–6 V), reduced SEL threshold (110 MeV·cm²/mg), identical TID rating (300 krad(Si)) and Flat-14 package. | Better suited for mixed-voltage systems (e.g., 3.3 V control + 5 V I/O); slightly lower heavy-ion margin acceptable in GEO or lunar orbit. | Choose when system-level radiation environment analysis confirms SEL margin is sufficient and wider supply flexibility is needed. |
Compared with RHFACT14K1, the 54ACT00 lacks flight certification documentation and lot-level radiation test reports, while RHFAC00 trades SEL immunity for broader voltage operation - making RHFACT14K1 the sole choice for LEO or MEO missions requiring maximum latch-up immunity and QML-V compliance.
Availability
RHFACT14K1 is available at Aetrix Electronics and suitable for onboard command decoder, satellite telemetry formatter, launch vehicle avionics sequencer, and deep-space probe power controller applications requiring stable component supply across extended production lifecycles and radiation-qualified continuity.
Supply support for RHFACT14K1 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
STMicroelectronics is a global semiconductor leader headquartered in Geneva, Switzerland, with dedicated rad-hard product lines serving defense, space, and nuclear instrumentation markets since 1985.
RHFACT14K1 belongs to ST's 54ACTxxx rad-hard logic family - engineered specifically for high-reliability digital control in spacecraft, launch systems, and strategic platforms where radiation-induced failures are unacceptable.
FAQ
Is RHFACT14K1 pin-compatible with standard 54ACT00 devices?
Yes - RHFACT14K1 uses the same Flat-14 pinout as generic 54ACT00 SMDs (MIL-PRF-38535), with identical terminal numbering, GND on Pin 7, and VCC on Pin 14. However, it includes additional QML-V screening, lot-level radiation test reports, and grounded-lid construction not present in commercial variants.
What is the maximum operating frequency of RHFACT14K1 at 5 V and 25 °C?
While no absolute maximum frequency is specified in the DB0998 summary, propagation delay is typically <10 ns per gate at VCC = 5 V and 25 °C. Based on SMD 5962F89547, maximum usable frequency in clean PCB layouts with 50 pF loads is ~35 MHz - derated further in high-dose or high-temperature conditions.
Does RHFACT14K1 require external decoupling capacitors?
Yes - a minimum 100 nF X7R ceramic capacitor must be placed within 2 mm of Pin 14 (VCC) and Pin 7 (GND) to suppress switching noise and maintain stable rail voltage during simultaneous output transitions, especially critical in rad-hard systems where transient-induced SEUs must be minimized.
Can RHFACT14K1 be used in circuits with 3.3 V logic interfaces?
No - RHFACT14K1 is an ACT-series device with TTL-compatible inputs requiring VIH ≥ 2.0 V, but its minimum VCC is 4.5 V. For 3.3 V systems, use the AC-series variant RHFAC00 (2–6 V operation) or add level-shifting circuitry; direct 3.3 V interfacing risks undefined logic states and increased susceptibility to noise.
RHFACT14K1 Specifications
- Product attributes
- Attribute value
- Manufacturer:
- STMicroelectronics
- Series:
- 54ACT
- Package/Case:
- 14-CFlatPack
- Packaging:
- Strip
- Product Status:
- Active
- Logic Type:
- Inverter
- Number of Circuits:
- 6
- Number of Inputs:
- 6
- Features:
- Schmitt Trigger
- Voltage - Supply:
- 4.5V ~ 5.5V
- Current - Quiescent (Max):
- -
- Current - Output High, Low:
- 24mA, 24mA
- Input Logic Level - Low:
- 0.8V
- Input Logic Level - High:
- 2V
- Max Propagation Delay @ V, Max CL:
- 12.5ns @ 4.5V, 50pF
- Operating Temperature:
- -55°C ~ 125°C
- Grade:
- -
- Qualification:
- -
- Mounting Type:
- Surface Mount
- Supplier Device Package:
- 14-CFlatpack
RHFACT14K1 FAQ
1.How can I place an order for RHFACT14K1 through Aetrix?
Please submit a Request for Quotation (RFQ) for RHFACT14K1 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 RHFACT14K1 reliable?
The price and inventory of RHFACT14K1 are updated periodically and may fluctuate due to market conditions. Stock and pricing data are typically refreshed every 24 hours. Quotation validity for RHFACT14K1 is usually 5 days.
3.What payment methods are accepted for RHFACT14K1?
We accept Wire Transfer, PayPal, Credit Card, Western Union, MoneyGram, and Escrow for RHFACT14K1 transactions.
Note: Certain payment methods may incur a processing fee.
4.How is shipping managed for RHFACT14K1?
RHFACT14K1 orders can be shipped via leading logistics carriers, including DHL, UPS, FedEx, TNT, or Registered Mail.
Once your RHFACT14K1 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 RHFACT14K1?
For technical support, including RHFACT14K1 datasheets, pinout diagrams, or application guidance, please contact our engineering support team. They can provide detailed documentation and assistance for your RHFACT14K1 requirements.
6.How does Aetrix verify that RHFACT14K1 is sourced from the original manufacturer or authorized distributors?
All RHFACT14K1 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 RHFACT14K1 meets industry standards.
7.What is the process for return or replacement of RHFACT14K1?
All RHFACT14K1 units undergo pre-shipment inspection (PSI). If there is an issue with RHFACT14K1, 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 RHFACT14K1 part is unused and in its original packaging.
Return procedure for RHFACT14K1:
1.Submit a request within 90 days.
2.Obtain a Return Material Authorization (RMA) from Aetrix.
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