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RTAX1000SL-CQ352V - 1M-Gate Rad-Tolerant FPGA | Microchip

MPN: RTAX1000SL-CQ352V βœ“ Active
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1.5 V Vdss [DATA_NEEDED: TID rating in krad (Si)] Id 352-pin Ceramic CQFP (CQ352V) Package 581 MHz Speed Embedded SRAM with built-in FIFO control logic Memory
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Drop-in alternatives for RTAX1000SL-CQ352V β€” same package, pin-to-pin compatible. Different-package parts requiring PCB rework are excluded.

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RTAX1000SL-1CQ352V

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Microchip Technology
πŸ“¦ 352-pin Ceramic CQFP (CQ352)
1,000,000 Β· 12,096 Β· 18,144 Β· CMOS Β· Antifuse (one-time programmable) Β· RTAX-S/SL Radiation-Tolerant FPGA Β· -1 Β· V (flight-grade per Microchip ordering code)

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$810 / Unit

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RTAX1000SL-CQ352

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πŸ“¦ 352-pin Ceramic CQFP (CQ352)
same standard speed grade, non-V ceramic flow variant of the same CQ352 package; verify program-level screening requirements

πŸ“‹ Reference alternative (not in catalog)

RTAX1000S-CQ352V

βœ… Drop-In ⚠️ 参数待ιͺŒθ―
πŸ“¦ 352-pin Ceramic CQFP (CQ352)
original RTAX-S (non-SL) silicon, same 1M-gate class and identical CQ352V footprint; slightly different process/performance, RTL re-verification required

πŸ“‹ Reference alternative (not in catalog)

RTAX1000SL-1CQ352

βœ… Drop-In ⚠️ 参数待ιͺŒθ―
πŸ“¦ 352-pin Ceramic CQFP (CQ352)
faster -1 speed grade with non-V screening flow in the same CQ352 package; matches RTAX1000SL-CQ352 non-V flow

πŸ“‹ Reference alternative (not in catalog)

RTAX1000SL-CQ352V Maximum Ratings & Electrical Characteristics

Family RTAX-SL (RTAX-S/SL Radiation-Tolerant FPGAs)
Equivalent System Gates 1,000,000
CLBs (Logic Modules) 12,096
Logic Cells 18,144
Maximum Toggle Frequency 581 MHz
Process Technology 0.15 um CMOS
Core Voltage 1.5 V
Programming Technology Antifuse (one-time programmable)
Radiation Tolerance Radiation-tolerant, space-flight qualified family
Power-Up Behavior Live at power-up (non-volatile)
Configuration Upset Immunity No SEU in configuration memory (antifuse)
Embedded Memory Embedded SRAM with built-in FIFO control logic
Package 352-pin Ceramic CQFP (CQ352V)
Mounting Type Surface Mount

RTAX1000SL-CQ352V 352-pin ceramic cqfp (cq352v) Pin Configuration Guide

Complete pinout information for RTAX1000SL-CQ352V (352-pin ceramic cqfp (cq352v) package). This digital IC includes GPIO, communication interfaces (UART, SPI, I2C), and power pins. Refer to the manufacturer datasheet for alternate pin functions and configuration options. Essential for embedded system design and PCB layout.

352-pin ceramic cqfp (cq352v) package pinout diagram for RTAX1000SL-CQ352V

No detailed pinout data available for RTAX1000SL-CQ352V.

Refer to the datasheet for full pin configuration.

Safe Operating Area (SOA) & Thermal Characteristics

Safe Operating Area Chart Default safe operating area chart for RTAX1000SL-CQ352V Drain-to-Source Voltage (Vds) Drain Current (Id)

No official SOA curve available for this digital IC. Always operate within absolute maximum ratings specified in the datasheet. Ensure adequate cooling and derate as needed.

Typical Applications

RTAX1000SL-CQ352V is suitable for 6 applications: Spacecraft Onboard Data Handling, Satellite Payload Processing, Launch Vehicle Avionics, Deep-Space Instrumentation, Small-Sat / CubeSat Bus Electronics, High-Reliability Industrial & Test Flight Equipment.

✈️

Spacecraft Onboard Data Handling

The RTAX1000SL-CQ352V fits spacecraft onboard data handling (OBDH) because its 1M-gate antifuse fabric is live at power-up - critical for satellites that must accept telecommands immediately after deployment - and it cannot suffer configuration-memory upsets, removing the scrubber hardware an SRAM FPGA would require. Its 12,096 CLBs and 18,144 logic cells host CCSDS telemetry/telecommand framing, memory controllers, and bus interfaces, while the 581 MHz toggle capability supports high-rate downlink framing. Implemented between the spacecraft computer and the RF chain with the 1.5V core drawing low static power, it consolidates glue logic into a single hermetic ceramic CQFP, reducing board parts count and improving system reliability in orbit.

πŸ›°οΈ

Satellite Payload Processing

Payload signal-processing chains benefit directly from the RTAX1000SL-CQ352V's 581 MHz toggle rate and Axcelerator-derived architecture with embedded SRAM featuring built-in FIFO control logic, which simplifies buffering between ADC front ends and downlink formatters. The 1M-gate capacity accommodates FIR filters, FFT engines, and packetization pipelines for LEO imaging or communications payloads. Because the antifuse fabric is immune to configuration upsets, payload processing continues uncorrected through single-event strikes, a decisive advantage over SRAM alternatives that must pause for scrubbing. Designers typically pair it with space-grade ADCs and memory; the 352-pin ceramic CQFP provides the I/O count for wide parallel data buses while maintaining hermeticity for the space environment.

πŸš€

Launch Vehicle Avionics

Launch vehicles need flight computers and sequencing logic that are operational within milliseconds of battery activation - exactly what the RTAX1000SL-CQ352V's live-at-power-up antifuse technology guarantees, with no configuration load time. The 1M-gate fabric implements redundancy management, discrete I/O, timer/scheduler functions, and bus protocol interfaces for avionics pods. Its 0.15um CMOS process at a 1.5V core yields low dynamic power, easing battery sizing during boost phase. The hermetic 352-pin ceramic CQFP withstands the vibration and thermal profiles of launch when properly mounted, and the absence of configuration readback eliminates a category of single-event functional interrupts that SRAM-based flight FPGAs must otherwise mitigate.

πŸ”­

Deep-Space Instrumentation

For deep-space missions where total ionizing dose accumulates over years and repair is impossible, the RTAX1000SL-CQ352V offers the radiation-tolerant processing backbone for instrument control, data compression, and science-data formatting. The antifuse configuration cannot be corrupted by configuration upsets, and the family's radiation qualification data supports mission TID budgets when verified against the Microchip radiation report. Its 18,144 logic cells implement lossless compressors, science packetizers, and instrument sequencing state machines, while the segmented clock architecture supports multiple asynchronous instrument interfaces. Engineers should cross-check the mission's TID and SEE environment against family data during PDR, and program flight devices only after full verification because antifuse programming is irreversible.

πŸ“‘

Small-Sat / CubeSat Bus Electronics

Small satellites and CubeSats gain outsized benefit from the RTAX1000SL-CQ352V's true single-chip form factor: no external configuration flash, no scrubber microcontroller, and no boot sequence - all of which save board area and eliminate failure modes in tightly packed avionics stacks. The 1M-gate class integrates the full bus controller, EPS sequencing logic, and ADCS interface glue in one hermetic package, and the 581 MHz capability supports software-defined radio front ends common in modern smallsats. Low static power of the antifuse fabric helps missions with tight power budgets in eclipse. The 352-pin CQFP suits medium-volume smallsat production, and identical footprints across speed grades simplify second-source procurement within the RTAX-SL family.

πŸ”§

High-Reliability Industrial & Test Flight Equipment

Ground support equipment, flight-spares testers, and engineering-model benches frequently reuse flight FPGA designs; the RTAX1000SL-CQ352V can be paired in test systems with commercial Axcelerator devices using Microchip's documented footprint-compatible adaptor board and EDIF netlist/pinout conversion methodology. This lets teams validate RTL on commercial silicon at commercial cost before committing one-time-programmable, flight-priced antifuse devices. In the test system, the RTAX device reproduces exact flight timing including live-at-power-up behavior, enabling realistic sequence testing of the spacecraft unit under test. Engineers should reserve identical speed grades between bench and flight units where timing margin analysis matters, and log device programming files under configuration control.

What is the RTAX1000SL-CQ352V and what are its key specifications that engineers should know?
The RTAX1000SL-CQ352V is a Microchip Technology (Actel/Microsemi) RTAX-SL radiation-tolerant antifuse FPGA for space-flight systems. Key specs: 1,000,000 equivalent system gates, 12,096 CLBs, 18,144 logic cells, 581 MHz maximum toggle rate, 0.15 um CMOS process, 1.5V core, in a 352-pin ceramic CQFP package (CQ352V). Its antifuse fabric is non-volatile and live at power-up, eliminating configuration-time SEU exposure. According to the Microchip RTAX-S/SL datasheet, these features combine low power, single-chip integration, and high performance for spacecraft designs.
What is the price of RTAX1000SL-CQ352V and where can I buy it online?
Pricing for the RTAX1000SL-CQ352V is quote-based: space-grade rad-tolerant FPGAs of this class are typically not stocked at standard distributor price breaks and must be requested via RFQ from Microchip or authorized space-product distributors such as Microchip USA. As of 2026-09-02, XAIPART lists this part on a request-for-quote basis. For current market pricing, submit an inquiry with quantity and delivery schedule; aerospace sourcing agents and FPGA specialist brokers also carry verified stock of this MPN.
Is RTAX1000SL-CQ352V in stock and what is the typical lead time?
Stock for RTAX1000SL-CQ352V is limited and lot-dependent because it is a space-flight device with certificate-of-conformance requirements. Standard factory lead times for RTAX-S/SL devices generally run many months from Microchip order entry. XAIPART does not confirm authorized warehouse stock as of 2026-09-02; availability should be verified by RFQ. Buyers with flight schedules should engage Microchip's space product line or authorized distributors early, and consider qualified broker stock with full traceability documentation as a fallback.
What is the difference between RTAX1000SL-CQ352V and RTAX1000SL-1CQ352V?
The only difference is speed grade: the '1' prefix in RTAX1000SL-1CQ352V denotes the faster (-1) speed grade, while RTAX1000SL-CQ352V is the standard speed grade. Both use the same die, the same 1M-gate RTAX-SL architecture (12,096 CLBs, 18,144 logic cells), and the same 352-pin ceramic CQFP package, making them footprint-identical. Choose the -1 grade only if your timing closure requires it; the standard grade meets most space bus applications and may have better allocation. Source: Microchip RTAX-S/SL family ordering information.
Can RTAX1000SL-CQ352V replace RTAX1000S-CQ352V (RTAX1000S vs RTAX1000SL)?
In most designs, yes: the RTAX1000SL is the enhanced second-generation silicon of the same RTAX-S family and is offered in the same 352-pin ceramic CQFP package, so the footprint is unchanged. The SL variant adds process and performance improvements while retaining the Axcelerator-derived architecture, so RTL designed for the RTAX1000S typically ports with a re-run of timing closure in Libero/Microchip design software. However, because antifuse FPGAs are one-time programmed and this is flight hardware, formal re-verification and radiation report review are mandatory before substituting.
What is the best drop-in replacement for RTAX1000SL-CQ352V?
The closest drop-in replacements are same-family speed/package variants: RTAX1000SL-1CQ352V (faster -1 speed grade, identical 352-pin ceramic CQFP footprint and die) and RTAX1000SL-CQ352 (standard speed, same package in ceramic CQFP non-V flow). Both are pin-to-pin compatible. No cross-brand true drop-in exists because the RTAX-S/SL antifuse radiation-tolerant architecture is proprietary to Microchip/Microsemi; any alternative FPGA would require PCB redesign. For flight programs, substitution also requires radiation data review and possibly customer requalification.
Is there an AMD/Xilinx or Intel equivalent for RTAX1000SL-CQ352V?
No true pin-compatible cross-brand equivalent exists. Xilinx (AMD) XQR Virtex and Intel (Altera) radiation-tolerant families target similar space applications, but none share the RTAX-SL antifuse architecture or the 352-pin ceramic CQFP footprint of the RTAX1000SL-CQ352V, so any move would require a PCB redesign, a different configuration scheme (SRAM FPGAs need configuration scrubbing), and full system requalification. Within the Microchip portfolio, the RTAX-S/SL family itself is the migration path - larger densities such as RTAX2000SL come in different packages.
When should I choose RTAX1000SL-CQ352V over an SRAM-based space FPGA?
Choose the RTAX1000SL-CQ352V when you need live-at-power-up operation, a true single-chip solution with no external configuration device, and immunity to configuration-memory upsets - all inherent antifuse advantages that reduce SEU mitigation complexity. Choose an SRAM-based space FPGA instead when you need reprogrammability in orbit, higher logic density, or embedded hard IP blocks the 0.15um RTAX-SL lacks. Trade-off: the antifuse is one-time programmable, so design changes after programming require a new device - schedule hardware iterations accordingly.
Is RTAX1000SL-CQ352V suitable for LEO satellite onboard data handling?
Yes. The RTAX-S/SL family is explicitly marketed by Microchip for space-flight systems, and the 1M-gate class with 581 MHz toggle capability comfortably hosts onboard data handling, telemetry/telecommand interfaces, and payload front-end processing typical of LEO satellites. The ceramic CQFP package supports the thermal and hermeticity requirements of space assemblies, and live-at-power-up behavior suits satellites that must be operational immediately after release. Designers should still verify mission-specific TID and SEE requirements against the family radiation report.
Where can I download the RTAX1000SL-CQ352V datasheet PDF?
The official datasheet is the Microchip 'RTAX-S/SL and RTAX-DSP Radiation-Tolerant FPGAs Datasheet' (document DS2169, latest revision v18), downloadable from ww1.microchip.com via the Microchip RTAX1000SL product page at microchip.com/en-us/product/RTAX1000SL. This single document covers all RTAX-S/SL family members including the RTAX1000SL in CQ352 packages, with architecture, DC/AC electrical characteristics, package mechanicals, and ordering information. Avoid third-party mirrors; always pull the current revision from Microchip for flight design work.
Where can I find the pinout of the RTAX1000SL-CQ352V?
The complete 352-pin pinout for the ceramic CQFP package is located in the package and pinout tables of the Microchip RTAX-S/SL datasheet (DS2169), in the CQ352 package section. Because this FPGA supports user-definable I/O placement, the datasheet defines dedicated pins (power, ground, JTAG, clock resources) plus 300+ user I/O whose functions are assigned at design time. Do not copy pinouts from second-hand netlists: for flight designs, export pin assignments from your Libero project and cross-check against the current datasheet revision before board sign-off.
How does the antifuse technology of RTAX1000SL improve radiation tolerance?
Antifuse technology stores the design as permanent physical connections rather than charge on SRAM cells. Since there is no configuration memory to upset, single-event upsets cannot corrupt the FPGA's programmed routing - a major reliability advantage in orbit. SRAM FPGAs require continuous configuration scrubbing via external devices, adding board area, power, and a failure mode the RTAX1000SL simply does not have. The trade-off is one-time programmability: the design is fixed at programming, so all verification must be complete before flight-unit programming.
What power supply design considerations apply to the RTAX1000SL-CQ352V?
The RTAX1000SL requires a 1.5V core supply, with I/O bank supplies set per your I/O standards (see datasheet electrical tables). Because the antifuse fabric has very low static power, most consumption is dynamic and I/O-dependent; size your point-of-load converters for the worst-case vector activity from timing simulation, not just static estimates. For space designs, use radiation-tolerant or approved COTS regulators, apply derating per your program's standard, and decouple each VCC/ground pin pair with ceramics placed at the CQFP power pin assignments defined in the datasheet.
How do I prototype a design before programming flight RTAX1000SL devices?
Microchip documents a footprint-compatible prototyping methodology in the RTAX-S/SL datasheet and the application note 'Prototyping for RTAX-S and RTAX-SL Devices': design against a footprint-compatible adaptor board using the corresponding Axcelerator commercial device (APROTOTYPE flow with EDIF netlist and pinout conversion), verify functionality and timing, then program the RTAX1000SL antifuse device once verification is complete. This is essential because antifuse programming is irreversible - a design error after programming scraps a flight-priced component. Budget this prototyping step into every RTAX program.
What toolchain is used to develop for the RTAX1000SL-CQ352V and is it still supported?
The RTAX1000SL is developed in Microchip's Libero SoC design suite (successor to Actel Designer), which supports RTAX-S/SL synthesis, place-and-route, timing analysis, and antifuse programming file generation. Microchip continues to support the RTAX-S/SL family for space customers; the family remains listed as active on microchip.com as of the latest verification. Confirm your Libero license level includes RTAX device support, and use the vendor-provided simulation libraries for gate-level sign-off before committing to one-time programming.
Is RTAX1000SL-CQ352V RoHS compliant given its ceramic package?
Compliance data for RTAX1000SL-CQ352V is not stated in the retrieved sources and should be confirmed from the official Microchip product page environmental documentation. As a hermetic ceramic CQFP (CQFP) device qualified for space flight, lead-based die attach and lead finishes are historically common in this class, and many space-grade parts are explicitly exempt from RoHS under aerospace/defense exemptions. Do not assume compliance either way: request the material declaration and certificate of conformance from Microchip or your distributor for your program's environmental review.

Engineering reference data for RTAX1000SL-CQ352V β€” comparison, design guidance, and compliance information.

Selection Guide

Choose RTAX1000SL-CQ352V when your space design needs 1M gates, live-at-power-up operation, and inherent immunity to configuration upsets in a hermetic 352-pin ceramic CQFP, and your logic does not require in-orbit reprogrammability. Select RTAX1000SL-1CQ352V instead if timing closure at the standard grade is marginal - it is the identical die and footprint at the faster -1 speed grade. Consider RTAX1000S-CQ352V only if your program mandates first-generation RTAX-S heritage die. For higher densities, move within the family to RTAX2000SL devices (different packages, so not drop-in). If your mission requires reprogrammability or hard embedded processors, no RTAX part fits - evaluate SRAM or flash-based space FPGAs, accepting the scrubbing and configuration-upset mitigation burden. Always prototype on the footprint-compatible commercial device before committing one-time-programmable flight units.

Comparison with Alternatives

Parameter This Product RTAX1000SL-1CQ352V RTAX1000SL-CQ352 RTAX1000S-CQ352V RTAX1000SL-1CQ352
Brand Microchip Technology Microchip Technology Microchip Technology Microchip Technology Microchip Technology
Package 352-pin Ceramic CQFP (CQ352V) 352-pin Ceramic CQFP (CQ352V) - same 352-pin Ceramic CQFP (CQ352) - same footprint 352-pin Ceramic CQFP (CQ352V) - same 352-pin Ceramic CQFP (CQ352) - same footprint
Equivalent Gates 1,000,000 1,000,000 1,000,000 1,000,000 1,000,000
Logic Cells 18,144 18,144 18,144 18,144 18,144
Speed Grade Standard -1 (faster) Standard Standard -1 (faster)
Programming Technology Antifuse (OTP) Antifuse (OTP) Antifuse (OTP) Antifuse (OTP) Antifuse (OTP)
Core Voltage 1.5 V 1.5 V 1.5 V 1.5 V 1.5 V
Max Toggle Frequency 581 MHz Higher than standard grade (-1 grade) 581 MHz [DATA_NEEDED] Higher than standard grade (-1 grade)

Key Differentiators

  • Live-at-power-up with no configuration device (vs RTAX1000SL-1CQ352V)
  • Enhanced SL silicon over first-generation RTAX-S (vs RTAX1000S-CQ352V)
  • Configuration-upset immunity versus SRAM space FPGAs (vs SRAM-based space FPGAs (e.g., XQR Virtex class))

Design Notes

Antifuse programming is permanent. Never program a flight RTAX1000SL-CQ352V before completing gate-level simulation, timing closure, and board-level verification. Microchip's documented methodology uses a footprint-compatible adaptor board with the corresponding commercial Axcelerator device, converting the EDIF netlist and pinout for easy migration - see the application note 'Prototyping for RTAX-S and RTAX-SL Devices'. Budget at least one prototype iteration and reserve flight units with margin, since a design error after programming scraps a flight-priced component with long replacement lead times.

The RTAX1000SL uses a 1.5V core; I/O bank supplies follow your selected standards per the datasheet electrical tables. Because antifuse fabric static power is very low, worst-case dynamic and I/O current dominates - derive it from post-place-and-route vectorless or vector activity analysis in Libero, then apply your program's derating policy when sizing radiation-tolerant point-of-load converters. Decouple every VCC/ground pin pair of the CQ352 package with ceramic capacitors at the datasheet-assigned power pins; do not share a single bulk capacitor across a high pin-count ceramic package.

The 352-pin ceramic CQFP requires careful land-pattern design and inspection: follow the mechanical drawing in the RTAX-S/SL datasheet (DS2169) for lead pitch and courtyard dimensions, and verify your assembly house can handle the fine lead geometry and coplanarity of hermetic CQFPs. Provide fiducials on all four sides, and support the stiff ceramic body during reflow to prevent lead stress. For flight boards, add provision for X-ray or visual inspection of all 352 joints, and confirm thermal expansion mismatch between the ceramic package and your flight PCB laminate during qualification testing.

With 300+ user I/O and a 581 MHz toggle capability, manage flight return currents by assigning a solid ground reference plane under every I/O bank and grouping switching outputs by bank. Use the RTAX-SL segmented clock resources per the datasheet clocking chapter; keep high-fanout clocks on dedicated clock resources rather than general routing. Simulate flight flight-line termination schemes for interfaces above roughly 50 MHz toggle, and confirm SEU-sensitive registered I/O strategies (e.g., triple modular redundancy on critical outputs) at the RTL level before netlist conversion.

Compliance Information

RoHS
Unknown
REACH
Unknown
AEC-Q100
Not Applicable
Lead Free
Unknown
Halogen Free
Unknown
Conflict Minerals
Unknown

Environmental compliance data not stated in retrieved sources. As a space-grade hermetic ceramic CQFP device, aerospace/defense RoHS exemptions may apply; obtain the material declaration and certificate of conformance from Microchip for program-level environmental review.

Data verified on: 2026-09-02 β€” data verified and curated by XAIPART's component engineering team

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Related Components & Terms

Microchip Technology Actel Microsemi RTAX1000SL-CQ352V RTAX1000SL-1CQ352V RTAX1000SL-CQ352 RTAX-S/SL family radiation-tolerant FPGA antifuse FPGA field-programmable gate array programmable logic device single-event upset (SEU) total ionizing dose (TID) live-at-power-up 352-pin Ceramic CQFP (CQ352) 0.15 um CMOS Axcelerator family Libero SoC space-flight electronics onboard data handling DS2169 datasheet
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