RTAX1000SL-CGS624B - 1M-Gate Rad-Tolerant FPGA CCGA-624 | Microchip
Teilenummer: RTAX1000SL-CGS624B ✓ Aktiv| Menge | Stückpreis | Gesamt |
|---|---|---|
| 1 | $1850 | $1.850,00 |
| 10 | $1720 | $17.200,00 |
| 100 | $1590 | $159.000,00 |
| 500 | $1480 | $740.000,00 |
| 1.000 | $1390 | $1.390.000,00 |
RTAX1000SL-CGS624B Übersicht
A radiation-tolerant FPGA is a field-programmable gate array engineered to survive the ionizing radiation environment of space flight, including total ionizing dose (TID) and single-event effects (SEE). Unlike commercial FPGAs, rad-tolerant FPGAs sit at the top of the programmable logic hierarchy (FPGA -> programmable logic IC -> digital IC -> semiconductor) and are qualified for satellite, planetary probe, and launch-vehicle electronics where replacement after deployment is impossible.
Key features include the anti-fuse-based RTAX-SL architecture derived from the commercial Axcelerator family, which provides live-at-power-up operation with no configuration device required. The embedded SRAM blocks include built-in FIFO control logic, and the fabric offers segmentable clocks and chip-wide highway routing for large system designs. Speed-grade B devices support system clock rates up to 581 MHz per family datasheets, with a 1.5V core supply.
The RTAX-SL fabric integrates embedded SRAM and bus-capable routing in a true single-chip form factor with low power consumption, making it suitable for payloads that must survive launch vibration and multi-year orbital missions. Design migration to RTAX-DSP variants is supported through the same development flow.
Typical applications include satellite payload data processing, spacecraft bus control, telemetry and telecommand (TT&C) interfaces, and instrument control in deep-space science missions.
A key design consideration: use Microchip Libero SoC with the RTAX-S prototyping methodology (footprint-compatible adaptor board plus EDIF netlist and pinout converter) to validate designs on commercial ProASIC/AX equivalents before committing to flight units.
This page synthesizes distributor availability data, same-family drop-in alternatives, and practical radiation-tolerant design notes not consolidated in the manufacturer datasheet.
Drop-in-Alternativen für RTAX1000SL-CGS624B – gleiches Gehäuse, Pin-kompatibel. Bauteile mit anderem Gehäuse, die eine PCB-Überarbeitung erfordern, sind ausgeschlossen.
Varianten dieser Serie
Modelle derselben Serie, die drop-in-kompatibel sind mit RTAX1000SL-CGS624B (gleiche Bauform und Footprint) – abweichend in Package, Family, Radiation Tolerance, ASIC Gates, Equivalent System Gates.
Schnellvergleichstool – Wählen Sie Alternativbauteile für den Direktvergleich:
RTAX1000SL-CGS624V
✅ Drop-In✓ Auf Lager
$3400 / Stück
Datenblatt ansehen →RTAX1000SL-CGS624E
✅ Drop-In✓ Auf Lager
$3970 / Stück
Datenblatt ansehen →RTAX1000SL-1CGS624B
✅ Drop-In✓ Auf Lager
$3200 / Stück
Datenblatt ansehen →RTAX1000SL-1CGS624E
✅ Drop-In✓ Auf Lager
$3420 / Stück
Datenblatt ansehen →RTAX2000SL-CGS624B
✅ Drop-In✓ Auf Lager
Preis auf Anfrage
Datenblatt ansehen →RTAX1000SL-CGS624B Grenzwerte & elektrische Eigenschaften
| Family | RTAX-S/SL Radiation-Tolerant FPGA |
| Equivalent System Gates | 1,000,000 gates |
| ASIC Gates | 125,000 gates |
| Combinational Cells (CLBs) | 12096 |
| Technology | 0.15 um CMOS, anti-fuse |
| Core Supply Voltage | 1.5 V |
| Maximum System Frequency | 581 MHz |
| Gehäuse | 624-pin CCGA (CGS624) |
| Speed Grade | B |
| Embedded SRAM | Yes, with built-in FIFO control logic |
| Configuration | Live-at-power-up (anti-fuse, single chip) |
| Clock Features | Segmentable clocks, chip-wide highway routing |
| Montageart | Surface Mount |
RTAX1000SL-CGS624B 624-pin ccga (cgs624) Pinbelegungsleitfaden
Pinbelegung für RTAX1000SL-CGS624B (624-pin ccga (cgs624)-Gehäuse). Dieser digitale IC umfasst GPIO, Kommunikationsschnittstellen (UART, SPI, I2C) und Versorgungspins. Alternative Pin-Funktionen und Konfigurationsoptionen entnehmen Sie dem Herstellerdatenblatt. Unverzichtbar für Embedded-System-Design und PCB-Layout.
Keine detaillierten Pinbelegungsdaten verfügbar für RTAX1000SL-CGS624B.
Siehe die Datenblatt für die vollständige Pin-Konfiguration.
Typische Anwendungen
RTAX1000SL-CGS624B ist geeignet für 6 Anwendungs: Satellite Payload Data Processing, Spacecraft Bus Control, Telemetry, Tracking & Command (TT&C), Deep-Space Science Instrument Control, Launch Vehicle Avionics, Earth Observation Imaging Chains.
Satellite Payload Data Processing
The RTAX1000SL-CGS624B fits payload processing chains that need 1M gates of reprogrammable logic plus embedded SRAM FIFOs in a single rad-tolerant chip. Its anti-fuse fabric is live at power-up, eliminating configuration-flash SEE concerns that plague SRAM FPGAs in orbit, and the 12,096 CLBs implement channelizers, FEC encoders, and framing engines. Placed between ADC/FPGA front ends and downlink modulators, its embedded SRAM with built-in FIFO control buffers high-rate science data without external memory, reducing parts count and board-level failure points. The 581 MHz B-grade fabric supports parallel datapaths at 100+ MHz real-world clock rates, and the CCGA-624 package's column interconnect withstands thermal cycling over multi-year LEO missions.
Empfohlen
Spacecraft Bus Control
Spacecraft bus controllers demand deterministic, always-on logic that survives total ionizing dose over mission life, which is exactly the RTAX-SL anti-fuse value proposition. The RTAX1000SL-CGS624B implements reaction-wheel interfaces, mode-state machines, and housekeeping telemetry with live-at-power-up operation so the FPGA is functional the instant the spacecraft separates from the launch vehicle - no configuration load delay. Its segmentable clocks and chip-wide highway routing support multiple independent functional domains (power, AOCS, TT&C) within one device. Low static power from the 1.5V core preserves battery energy during eclipse operations, and the CCGA-624 ceramic package provides hermetic environmental protection for vacuum operation.
Empfohlen
Telemetry, Tracking & Command (TT&C)
TT&C subsystems benefit from the RTAX1000SL-CGS624B's combination of 1M gates and deterministic anti-fuse timing with no configuration-upset risk from single-event effects. Designers implement CCSDS framing, convolutional and Reed-Solomon encoders/decoders, and command decoders in the 12,096-CLB fabric, while embedded SRAM blocks with FIFO control handle rate buffering between the baseband and RF sections. Because the device is configured at manufacture (one-time programmable), TT&C logic cannot be corrupted in flight - a critical reliability property for the link that commands the spacecraft. The B speed grade's 581 MHz ceiling comfortably covers typical TT&C symbol rates with parallelism margin.
Empfohlen
Deep-Space Science Instrument Control
Deep-space instruments such as spectrometers and imagers require logic that tolerates high TID behind minimal shielding, and the RTAX1000SL-CGS624B addresses this with its rad-tolerant 0.15 um CMOS anti-fuse process. Instrument sequencers, ADC interface logic, and on-board compression engines fit within the 1M-gate / 125,000 ASIC-gate capacity, with embedded SRAM FIFOs absorbing burst data from sensor arrays. True single-chip operation (no external configuration device) reduces the parts exposed to the radiation environment. Engineers should budget SEU mitigation via triple-module redundancy in the fabric, and use the Microchip prototyping methodology on commercial Axcelerator parts before committing flight units.
Empfohlen
Launch Vehicle Avionics
Launch-vehicle flight computers and stage controllers use the RTAX1000SL-CGS624B where short but severe missions demand guaranteed live-at-power-up behavior and vibration-tolerant column-grid packaging. The CCGA-624 ceramic package's column interconnect resists mechanical shock during stage separation better than fine-pitch commercial BGAs, and the anti-fuse fabric needs no boot sequence during the seconds-critical launch timeline. The 1M-gate fabric implements GN&C glue logic, redundant-voter circuits, and telemetry multiplexers, while segmentable clocks let designers partition safety-critical and non-critical functions with independent timing domains. DLA-qualified variants of the RTAX1000SL family exist under Mil-Prf-38535 Class V per Microchip's DLA cross-reference guide.
Empfohlen
Earth Observation Imaging Chains
Earth-observation satellites route high-rate imager data through the RTAX1000SL-CGS624B, which provides enough 12,096-CLB capacity for CCD/CMOS sensor interface, defect correction, and lossless pre-compression in one rad-tolerant chip. Embedded SRAM with FIFO control logic buffers line data between the sensor clock domain and the mass-memory downlink domain without external FIFO ICs. The device's low power consumption matters because imaging payloads are power-budget-critical in orbit, and live-at-power-up anti-fuse configuration ensures the imager is ready at first acquisition. For higher-resolution instruments, the same-package RTAX2000SL-CGS624B doubles logic capacity with zero board redesign.
Empfohlen
Zusammenfassung der empfohlenen Produkte
Technische Referenzdaten für RTAX1000SL-CGS624B – Vergleich, Designhinweise und Compliance-Informationen.
Auswahlhilfe
Vergleich mit Alternativen
| Parameter | Dieses Produkt | RTAX1000SL-CGS624V | RTAX1000SL-CGS624E | RTAX1000SL-1CGS624B | RTAX2000SL-CGS624B |
|---|---|---|---|---|---|
| Package | 624-pin CCGA (CGS624) | 624-pin CCGA (CGS624) - same | 624-pin CCGA (CGS624) - same | 624-pin CCGA (CGS624) - same | 624-pin CCGA (CGS624) - same |
| Brand | Microchip Technology | Microchip Technology | Microchip Technology | Microchip Technology | Microchip Technology |
| Equivalent System Gates | 1,000,000 | 1,000,000 | 1,000,000 | 1,000,000 | 2,000,000 |
| CLBs (Cells) | 12096 | 12096 | 12096 | 12096 | 21504 |
| Speed Grade | B | V | E | B | B |
| Core Supply Voltage | 1.5 V | 1.5 V | 1.5 V | 1.5 V | 1.5 V |
| Configuration | Anti-fuse, live-at-power-up (single chip) | Anti-fuse, live-at-power-up | Anti-fuse, live-at-power-up | Anti-fuse, live-at-power-up | Anti-fuse, live-at-power-up |
Wichtigste Unterscheidungsmerkmale
- 1M-gate density in the flight-proven RTAX-SL anti-fuse family (vs. RTAX250SL-CG624B)
- Pin-compatible upgrade path without board redesign (vs. RTAX2000SL-CGS624B)
- Live-at-power-up single-chip operation vs SRAM FPGAs (vs. RTAX1000SL-CGS624V)
Designhinweise
The CGS624 CCGA uses solder columns rather than solder balls, so the land pattern must be designed for column pitch with adequate fillet volume; follow the RTAX-S/SL datasheet package mechanical drawing. Columns mechanically decouple the ceramic substrate from PCB thermal-expansion mismatch, which is essential across the large temperature swings of orbital missions. Avoid routing high-speed signals directly under the package center without a ground plane, and verify board warpage specs meet the ceramic package flatness requirement before reflow profiling.
RTAX-S devices are one-time programmable anti-fuse FPGAs - there is no rework path after programming. Complete full timing closure, functional verification, and pin assignment sign-off in Microchip Libero SoC before sending flight units to programming. Use the manufacturer's prototyping methodology (footprint-compatible adaptor board on commercial Axcelerator parts plus EDIF netlist and pinout conversion) to shake out design bugs on cheap commercial silicon first, per the application note 'Prototyping for RTAX-S and RTAX-SL Devices'.
Estimate: budget the 1.5V core supply per the RTAX-S/SL datasheet power calculator with your actual toggle rates, since fabric power scales with switching activity and the 1M-gate fabric can draw substantial current at high utilization. Provide independent clean rails for core and I/O banks with bulk plus 0.1uF decoupling at each supply pin group. Ensure power-up ramp meets datasheet monotonicity requirements - anti-fuse devices must be live and configured correctly at first power application.
With 624 I/O available in the CGS624 package, group I/O banks by voltage standard and keep simultaneously switching outputs distributed across banks to limit ground bounce on the ceramic substrate. Simulate flight harness-driven lines for reflection and crosstalk, and reserve spare pins for mitigated (TMR-replicated) signals in SEU-critical paths. Match trace lengths within source-synchronous buses such as ADC or DDR-style interfaces to the datasheet setup/hold budgets for the B speed grade.
Compliance-Informationen
Space-flight hermetic ceramic package (CCGA); DLA-qualified variants of the RTAX1000SL family exist under DLA standard microcircuit drawings per Microchip's DLA Cross Reference Guide (Mil-Prf-38535 QML Class Q/V). Specific RoHS/REACH status for this exact ordering code not stated in provided data.
