RTAX250S-LG624EV - 250K Gate Rad-Tolerant FPGA | Microchip
部品番号: RTAX250S-LG624EV ✓ 生産中| 数量 | 単価 | 小計 |
|---|---|---|
| 1 | $0 | $0.00 |
| 10 | $0 | $0.00 |
| 100 | $0 | $0.00 |
| 500 | $0 | $0.00 |
| 1,000 | $0 | $0.00 |
RTAX250S-LG624EV 概要
A radiation-tolerant FPGA is a field-programmable gate array engineered to survive the total ionizing dose (TID) and single-event effects (SEE) found in orbital and deep-space radiation environments. Within the power-management and processing hierarchy of a spacecraft avionics system, the FPGA sits between a radiation-hardened microcontroller and application-specific ASICs, providing flexible glue logic, bus interfacing, and payload processing. The RTAX-S family is the successor to the Actel Axcelerator-based architecture, now manufactured and supported by Microchip (formerly Microsemi).
Key features include true single-chip operation with live-at-power-up functionality enabled by the anti-fuse interconnect, which requires no configuration PROM and eliminates configuration-time vulnerability to radiation-induced SEUs in configuration memory. The device integrates embedded SRAM blocks, clock management circuitry, and up to 248 user I/Os in the 624-pin package, with industrial temperature capability spanning -55C to +125C in the EV-grade flow.
Architecturally, the RTAX250S combines Sea-of-Modules logic tiles with VersaTiles and dedicated embedded memory blocks, delivering high routing efficiency and deterministic timing. The 0.15 um anti-fuse process provides low static power and inherent immunity to configuration upsets, a decisive advantage over SRAM-based FPGAs in space applications.
Typical applications include satellite attitude-control and payload data processing, spaceflight bus interfaces such as Mil-Std-1553 and SpaceWire bridges, and telemetry/command (TM/TC) systems where single-chip, live-at-power-up logic is mandatory.
Design consideration: because RTAX-S devices are one-time programmable, complete design verification using the Microchip Libero design flow and, where possible, Aldec flash-based prototyping adaptor boards is strongly recommended before committing hardware.
This page synthesizes verified distributor data, drop-in packaging variants, and design guidance not consolidated in the manufacturer datasheet. Pricing is quote-based as of 2026-09-02.
ドロップイン代替品: RTAX250S-LG624EV — 同一パッケージでピン互換。PCBの作り直しが必要な異なるパッケージの部品は除外されています。
このシリーズのバリエーション
同一シリーズでドロップイン互換のモデル: RTAX250S-LG624EV （同一形状・フットプリント） — 相違点: Radiation Tolerance, Family, Package, Configuration, Process Technology.
クイック比較ツール — 並列比較する代替部品を選択:
RTAX250S-LG624V
✅ ドロップイン✓ 在庫あり
価格はお問い合わせください
データシートを見る →RTAX250S-LG624B
✅ ドロップイン✓ 在庫あり
$2350 / 個
データシートを見る →RTAX250S-1LG624V
✅ ドロップイン✓ 在庫あり
価格はお問い合わせください
データシートを見る →RTAX250SL-LG624V
✅ ドロップイン✓ 在庫あり
$1620 / 個
データシートを見る →RTAX250SL-LG624E
✅ ドロップイン✓ 在庫あり
$1000 / 個
データシートを見る →RTAX250SL-1LG624V
✅ ドロップイン✓ 在庫あり
$950 / 個
データシートを見る →RTAX250SL-LG624B
✅ ドロップイン✓ 在庫あり
$2380 / 個
データシートを見る →RTAX250S-CG624E
✅ ドロップイン✓ 在庫あり
価格はお問い合わせください
データシートを見る →RTAX250S-LG624EV 最大定格＆電気的特性
| Family | RTAX-S Radiation-Tolerant FPGA |
| Equivalent Gate Count | 250,000 gates |
| Logic Cells | 4224 |
| Configurable Logic Blocks (CLBs) | 2816 |
| User I/Os | 248 |
| Core Supply Voltage | 1.5 V nominal |
| Maximum System Frequency | 649 MHz |
| Process Technology | 0.15 um CMOS anti-fuse |
| Programming Technology | Anti-fuse (one-time programmable), live at power-up |
| パッケージ | 624-pin LGA |
| 実装タイプ | Surface Mount |
| 動作温度 | -55C to +125C |
| Radiation Tolerance | Radiation-tolerant (space-flight qualified family) |
| Application Grade | Space / hi-rel |
| Configuration Device Required | No (single-chip, live at power-up) |
RTAX250S-LG624EV 624-pin lga ピン配置ガイド
RTAX250S-LG624EV (624-pin lga パッケージ) のピン配置。 このデジタルICには、GPIO、通信インターフェース (UART、SPI、I2C)、および電源ピンが含まれています。代替ピン機能と設定オプションについては、メーカーのデータシートを参照してください。組み込みシステム設計とPCBレイアウトに不可欠です。
詳細なピン配置データはありません: RTAX250S-LG624EV.
詳細は データシート をご参照ください。
主な用途
RTAX250S-LG624EV の用途: 6 件s: Satellite Payload Data Processing, Spacecraft Bus Interface and Bridge Logic, Telemetry, Tracking and Command (TM/TC), Attitude Determination and Control Systems (ADCS), Spaceflight Instrument Sequencing and Timing, Launch Vehicle Avionics Logic.
Satellite Payload Data Processing
The RTAX250S-LG624EV fits payload data-processing chains where radiation tolerance and deterministic single-chip operation dominate. Its 250K gates and 4224 logic cells implement framing, FIFO buffering, and CCSDS-formatting logic, while 248 user I/Os interface payload sensors and downlink modems. Because the anti-fuse fabric is live at power-up, the payload logic is available the instant the spacecraft power bus energizes, with no configuration PROM to fail or suffer configuration SEUs. The 1.5V core keeps static power low, a key budget line on power-constrained small satellites, and the 624-pin LGA provides the I/O density needed for wide parallel payload buses.
おすすめ
Spacecraft Bus Interface and Bridge Logic
Spacecraft command and data handling (CDH) systems use the RTAX250S-LG624EV as glue logic between legacy buses such as Mil-Std-1553, CAN, and SpaceWire and modern payload processors. The 649 MHz class architecture easily closes timing for bus codec cores, while the 248 I/Os support multiple concurrent interfaces. The radiation-tolerant anti-fuse fabric avoids the configuration-upset mitigation (triple modular redundancy of configuration memory) that SRAM FPGAs require in orbit, simplifying fault management. With a -55C to +125C EV-grade range, the device tolerates the thermal cycling of eclipse transitions without derating the interface timing.
おすすめ
Telemetry, Tracking and Command (TM/TC)
TM/TC modules demand fail-safe, always-available logic: decoders for uplink commands, formatters for housekeeping telemetry, and watchdog functions. The RTAX250S-LG624EV is well suited because its configuration is fixed at programming time, so a radiation-induced configuration upset cannot disable the command decoder - a decisive safety property versus SRAM-based FPGAs. The device's live-at-power-up behavior guarantees the receiver chain is decoding commands the moment power is applied, and its 2816 CLBs provide ample capacity for convolutional or Reed-Solomon-adjacent framing support functions in the 624-pin LGA footprint.
おすすめ
Attitude Determination and Control Systems (ADCS)
ADCS electronics interface star trackers, sun sensors, gyroscopes, and reaction-wheel drivers - a mix of parallel, serial, and PWM signals that the RTAX250S-LG624EV handles with its 248 user I/Os and flexible I/O standards. The 250K-gate capacity hosts sensor-fusion preprocessing and the wheel-driver PWM generators, while deterministic anti-fuse routing ensures consistent control-loop latency, important for stable pointing budgets. Its low 1.5V core supply and low static power fit the continuous-duty profile of ADCS electronics, and the -55C to +125C range covers the thermal environment of external equipment panels.
おすすめ
Spaceflight Instrument Sequencing and Timing
Scientific instruments on orbital platforms require precision sequencers that trigger detectors and digitizers with sub-microsecond determinism. The RTAX250S-LG624EV implements these sequencers in its 649 MHz-class fabric, with on-chip memory blocks buffering readout streams. Because the design is hardened into anti-fuse interconnect at programming time, the timing is fixed and repeatable across the mission - no reconfiguration jitter or boot-time gaps between observation windows. The EV temperature grade supports instruments exposed to -55C to +125C, and the single-chip 624-pin LGA saves board area inside tight instrument housings.
おすすめ
Launch Vehicle Avionics Logic
Launch vehicles impose extreme vibration, wide temperature, and short mission durations where configuration reliability is paramount. The RTAX250S-LG624EV's anti-fuse fabric withstands vibration mechanically (no soldered configuration PROM to shed) and logically (no configuration upsets), making it a common choice for flight-event sequencers, redundant-voting logic, and range-safety interface bridges. The 248 I/Os terminate discrete and MIL-STD interfaces, and live-at-power-up operation ensures the flight computer's peripheral logic is active from umbilical power application through stage separation, with -55C to +125C operation across the flight thermal profile.
おすすめ
おすすめ製品の概要
エンジニアリング参考データ: RTAX250S-LG624EV — 比較、設計ガイダンス、コンプライアンス情報。
選定ガイド
代替品との比較
| パラメータ | この製品 | RTAX250S-LG624V | RTAX250S-LG624B | RTAX250S-1LG624V | RTAX250SL-LG624V | RTAX250S-CG624E |
|---|---|---|---|---|---|---|
| Package | 624-pin LGA | 624-pin LGA - same | 624-pin LGA - same | 624-pin LGA - same | 624-pin LGA - same | 624-pin ceramic package - same position map |
| Brand | Microchip Technology | Microchip Technology | Microchip Technology | Microchip Technology | Microchip Technology | Microchip Technology |
| Equivalent Gates | 250,000 | 250,000 | 250,000 | 250,000 | 250,000 | 250,000 |
| Logic Cells / CLBs | 4224 / 2816 | 4224 / 2816 | 4224 / 2816 | 4224 / 2816 | 4224 / 2816 | 4224 / 2816 |
| Speed Grade | Standard | Standard | Standard | -1 (faster) | Standard (SL process) | Standard |
| Core Supply Voltage | 1.5 V | 1.5 V | 1.5 V | 1.5 V | 1.5 V | 1.5 V |
| Static Power Profile | Standard RTAX-S | Standard RTAX-S | Standard RTAX-S | Standard RTAX-S | Lower static power (SL) | Standard RTAX-S |
主な差別化要因
- True single-chip, live-at-power-up operation （vs RTAX250SL-LG624V)
- Faster timing margin available on identical footprint （vs RTAX250S-1LG624V)
- Lower static power option on same die （vs RTAX250SL-LG624V)
- Trade-off: ceramic package variant needs land-pattern review （vs RTAX250S-CG624E)
設計ノート
RTAX-S devices are one-time programmable. Never submit a design to the programming center without exhaustive simulation, static timing analysis in Microchip Libero, and a formal design review. The manufacturer-recommended methodology is prototyping on the Aldec flash-based RTAX adaptor (ProASIC3E technology) using the footprint-compatible adaptor board with an EDIF netlist and pinout converter described in the Microchip application note 'Prototyping for RTAX-S and RTAX-SL Devices'. Any post-programming change requires a new device - budget spare units accordingly.
Provide a clean 1.5V core rail with decoupling per the Microchip RTAX-S power guidelines: bulk capacitance at the regulator and distributed 0.1 uF ceramics at the LGA power pins. If power budget is tight, consider the RTAX250SL variants, which use a low-power process option to cut static current on the same footprint. I/O bank voltages must match the connected bus standards; verify bank assignment in the Libero pin editor before PCB routing because the OTP device cannot tolerate pin swaps after layout freeze.
The 624-pin LGA requires a precision land pattern per the Microchip RTAX-S datasheet package section, with matched pad geometry to ensure coplanarity across the large body. Use a defined reflow profile with x-ray inspection capability for flight hardware, and avoid hand rework of LGA devices. Dedicate escape vias per signal pad where fanout is dense; the 248 user I/Os frequently require high-layer-count boards. Do not route noisy switching-regulator nodes under the package.
For high-rate interfaces approaching the 649 MHz-class fabric performance, use the '-1' speed grade part (e.g., RTAX250S-1LG624V) to secure timing margin, and control trace impedance per the bus standard requirements. Series-terminate single-ended outputs to contain overshoot on long backplane runs, and keep clock pairs short and referenced to a solid ground plane. Confirm final timing with Libero static timing analysis at the -55C to +125C corner, not just room temperature.
コンプライアンス情報
Space-grade hi-rel device; compliance declarations are program-specific and must be obtained from Microchip with the certificate of conformance. Not an automotive AEC-Q100 product.
