RTAX2000S-CQ256PROTO - 2M-Gate Rad-Tolerant FPGA Prototype | Microchip
Артикул: RTAX2000S-CQ256PROTO ✓ Активен| Кол-во | Цена за ед. | Итого |
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| 1 | $0 | $0,00 |
| 10 | $0 | $0,00 |
| 100 | $0 | $0,00 |
| 500 | $0 | $0,00 |
| 1.000 | $0 | $0,00 |
RTAX2000S-CQ256PROTO Обзор
A radiation-tolerant FPGA (Field Programmable Gate Array) is a programmable logic device engineered to survive the ionizing radiation environments of space flight, including total ionizing dose (TID), single-event upset (SEU), and single-event latchup (SEL). Within the power hierarchy of spacecraft electronics, the RTAX-S family sits alongside rad-hard processors and memory as core onboard data-processing silicon, using anti-fuse programmable interconnect that is programmed once and remains stable under radiation.
Key features of the RTAX2000S-CQ256PROTO include low-power consumption, true single-chip form factor, and live-at-power-up (LAPU) operation, which eliminates the need for an external configuration device. The PROTO variant shares the same functional characteristics as the space flight unit but ships in a non-hermetic package at a fraction of the cost, specifically for functional verification before committing to flight parts.
Architecturally, the RTAX-S/SL family uses Microchip's Axcelerator-derived logic fabric with a sea-of-modules architecture combining C-cells, R-cells, and embedded SRAM/dedicated FIFO blocks, enabling high performance at densities up to four million equivalent system gates for space-based applications.
Typical applications include satellite on-board data handling, spacecraft payload processing, telemetry and telecommand interfaces, and reprogrammable prototyping of RTAX-S flight designs. Designers often pair the PROTO device with Aldec prototyping adaptors that map ProASIC3E flash technology onto the CQ256 footprint for iterative functional verification.
A key design consideration is that PROTO devices are non-hermetic and not radiation-screened, so they must never be flown; they exist solely for de-risking the flight design. Timing closure performed on PROTO silicon should be re-verified against flight-grade specifications.
This page synthesizes distributor availability, drop-in alternatives, and practical design notes not found in the manufacturer datasheet.
Аналоги без доработки для RTAX2000S-CQ256PROTO — тот же корпус, pin-to-pin совместимость. Компоненты в других корпусах, требующие переработки PCB, исключены.
Варианты в этой серии
Модели той же серии, совместимые без доработки с RTAX2000S-CQ256PROTO (тот же форм-фактор и посадочное место) — отличается по Package, Configuration, Radiation Tolerance, Technology, Embedded Memory.
Инструмент быстрого сравнения — выберите альтернативные компоненты для сравнения бок о бок:
RTAX2000S-1CQ256PROTO
✅ Прямая замена✓ В наличии
$1595 / шт.
Открыть даташит →RTAX2000SL-CQ256V
✅ Прямая замена✓ В наличии
Уточнить цену
Открыть даташит →RTAX2000SL-1CQ256PROTO
✅ Прямая замена✓ В наличии
Уточнить цену
Открыть даташит →RTAX2000S-CQ256V
✅ Прямая замена✓ В наличии
Уточнить цену
Открыть даташит →RTAX2000SL-1CQ256V
✅ Прямая замена✓ В наличии
Уточнить цену
Открыть даташит →RTAX2000S-CQ256PROTO Максимальные параметры и электрические характеристики
| System Gates | 2,000,000 |
| Configurable Logic Blocks (CLBs) | 21504 |
| Maximum System Frequency | 350 MHz |
| User I/Os | 136 |
| Process Technology | CMOS |
| Корпус | CQFP-256 (ceramic quad flat pack, 256 pins) |
| Device Type | PROTO (prototype, non-hermetic package, same functional characteristics as flight unit) |
| Radiation Tolerance | Radiation-tolerant family (RTAX-S) - flight screening applies to hermetic V variants only |
| Programmable Interconnect | Anti-fuse (one-time programmable) |
| Configuration | Live at power-up (LAPU), no external configuration device required |
| Family | RTAX-S/SL Radiation-Tolerant FPGAs |
| Тип монтажа | Surface Mount |
| Primary Application Domain | Space-flight systems |
| Qualification Grade | PROTO (non-hermetic; not for flight use) |
Руководство по цоколевке RTAX2000S-CQ256PROTO в корпусе cqfp-256 (ceramic quad flat pack, 256 pins)
Цоколевка для RTAX2000S-CQ256PROTO (корпус cqfp-256 (ceramic quad flat pack, 256 pins)). Эта цифровая ИС включает выводы GPIO, интерфейсы связи (UART, SPI, I2C) и выводы питания. Обратитесь к техническому описанию производителя для альтернативных функций выводов и вариантов конфигурации. Необходимо для проектирования встраиваемых систем и трассировки печатных плат.
Нет подробных данных о распиновке для RTAX2000S-CQ256PROTO.
Обратитесь к даташиту для полной конфигурации выводов.
Типичное применение
RTAX2000S-CQ256PROTO подходит для 6 применениеs: Satellite On-Board Data Handling, Payload Signal Processing, Reprogrammable Prototyping with Aldec Adaptors, Telemetry and Telecommand Interfaces, Launch Vehicle Avionics, Space Instrumentation and Sensor Front Ends.
Satellite On-Board Data Handling
The RTAX2000S-CQ256PROTO fits satellite on-board computer and data-handling subsystems where 2,000,000 system gates of glue logic, bus interfaces, and control functions must be consolidated in a single live-at-power-up device. Its 21,504 CLBs integrate memory controllers, CCSDS framing, and bus bridges that would otherwise require multiple rad-tolerant ASICs, and the 136 user I/Os cover MIL-STD-1553, SpaceWire-class, and low-rate telemetry interfaces. Designers first validate the full data-handling HDL on the low-cost PROTO unit, exploiting identical functional characteristics to the flight die, then transfer to the hermetic CQ256V flight part without PCB respin. Because the anti-fuse fabric needs no external configuration PROM, the design powers up instantly at spacecraft switch-on.
Рекомендуется
Payload Signal Processing
For payload preprocessing chains - FFT pre-filtering, format conversion, and sensor-interface aggregation - the RTAX2000S-CQ256PROTO offers a 350 MHz-class fabric with 21,504 CLBs, enough to host pipelined DSP datapaths alongside interface logic in one radiation-tolerant device. The PROTO device's non-hermetic package keeps prototype cost down while its functionally identical flight die ensures that timing closure and resource utilization results carry over to the flight build. Embedded SRAM blocks implement line buffers and coefficient storage, while the 136 user I/Os connect ADCs and downlink formatters. Teams typically iterate payload algorithms on Aldec ProASIC3E-based adaptors, then commit the verified netlist to the one-time-programmable PROTO part for board-level validation.
Рекомендуется
Reprogrammable Prototyping with Aldec Adaptors
The RTAX2000S-CQ256PROTO is the natural target for Aldec's RTAX prototyping solution, which maps flash-based Microchip ProASIC3E devices onto the CQ208, CQ256, CQ352, and CG624 RTAX footprints. In this flow, engineers develop and debug against the reprogrammable ProASIC3E adaptor, then program the anti-fuse PROTO device to verify the exact production silicon behavior, since PROTO parts carry the same functional characteristics as the flight unit per Microchip's AC170 application note. This two-stage approach de-risks one-time-programmable commitment: any HDL or pinout error surfaces before the final anti-fuse build. The PROTO's CQ256 footprint matches the flight CQ256V exactly, so the completed validation PCB feeds directly into flight assembly.
Рекомендуется
Telemetry and Telecommand Interfaces
Spacecraft TT&C chains demand deterministic, always-on logic from the instant the spacecraft powers up - exactly what the RTAX2000S-CQ256PROTO's live-at-power-up anti-fuse architecture provides, with no configuration time and no single-point configuration-memory failure mode. Its 2,000,000 gates accommodate command decoders, packetizers, time-tag distribution, and redundant cross-strapping among 136 user I/Os, allowing one device to replace several rad-tolerant ASSPs. Prototyping on the CQ256PROTO lets teams verify CCSDS-compliant frame formats and majority-voted command paths on production-equivalent silicon before ordering hermetic flight units. Low static power consumption of the CMOS fabric suits eclipse-mode operation where TT&C logic must remain energized.
Рекомендуется
Launch Vehicle Avionics
Launch-vehicle flight-control and sequencing electronics need high gate counts and short, deterministic paths - the RTAX2000S-CQ256PROTO's 21,504 CLBs and 350 MHz-class fabric host redundant voter logic, motor-control sequencers, and range-safety interfaces with ample timing margin. Ground-segment avionics test benches frequently employ the low-cost PROTO device to exercise the exact netlist that will fly, since Microchip documents that PROTO parts match flight-unit functional characteristics; only the hermetic package and screening differ. The 136 user I/Os handle quadrature feedback, discrete discretes, and redundant serial links, and the single-chip form factor reduces connector count and board area in densely packaged avionics bays. Migration to RTAX2000S-CQ256V requires no board change.
Рекомендуется
Space Instrumentation and Sensor Front Ends
Scientific instruments - star trackers, spectrometers, radiation monitors - use the RTAX2000S-CQ256PROTO to prototype detector timing generators, histogram engines, and housekeeping aggregation in one 2,000,000-gate device. The live-at-power-up fabric ensures the instrument is operational at first light after deployment without a boot sequence, a decisive advantage over SRAM FPGAs vulnerable to configuration upsets at power-on. With 136 user I/Os, the device links directly to CCD/CMOS imagers and ADCs while reserving channels for redundant telemetry. Instrument teams exploit the PROTO's functional identity with the flight die to validate acquisition scripts and timing on real silicon, then order the hermetic RTAX2000SL-CQ256V for flight, keeping the same CQ256 footprint and package outline.
Рекомендуется
Сводка рекомендуемых товаров
Справочные инженерные данные для RTAX2000S-CQ256PROTO — сравнение, рекомендации по проектированию и информация о соответствии.
Руководство по выбору
Сравнение с аналогами
| Параметр | Этот товар | RTAX2000S-1CQ256PROTO | RTAX2000SL-CQ256V | RTAX2000S-CQ256V | RTAX2000SL-1CQ256V |
|---|---|---|---|---|---|
| Package | CQFP-256 (non-hermetic PROTO) | CQFP-256 (non-hermetic PROTO) - same | CQFP-256 (hermetic V) - same footprint | CQFP-256 (hermetic V) - same footprint | CQFP-256 (hermetic V) - same footprint |
| Brand | Microchip Technology | Microchip Technology | Microchip Technology | Microchip Technology | Microchip Technology |
| System Gates | 2,000,000 | 2,000,000 | 2,000,000 | 2,000,000 | 2,000,000 |
| CLBs | 21504 | 21504 | 21504 | 21504 | 21504 |
| User I/Os | 136 | 136 | 136 | 136 | 136 |
| Speed Grade | Base (fastest) | -1 (standard) | Base (SL process) | Base | -1 (SL process) |
| Qualification Level | PROTO (non-hermetic, not for flight) | PROTO (non-hermetic, not for flight) | Flight-grade (hermetic V) | Flight-grade (hermetic V) | Flight-grade (hermetic V) |
| Process Variant | RTAX-S | RTAX-S | RTAX-SL (improved speed/power) | RTAX-S | RTAX-SL (improved speed/power) |
| Configuration | Anti-fuse, live at power-up | Anti-fuse, live at power-up | Anti-fuse, live at power-up | Anti-fuse, live at power-up | Anti-fuse, live at power-up |
Ключевые отличия
- Low-cost functional verification of flight silicon (против RTAX2000S-CQ256V)
- Fastest speed grade in the same footprint (против RTAX2000S-1CQ256PROTO)
- Improved process available via SL variant (против RTAX2000SL-CQ256V)
Заметки по проектированию
Never fly the PROTO device. Per Microchip application note AC170, RTAX-S/SL PROTO parts share the flight unit's functional characteristics but use a non-hermetic package and lack the radiation screening and qualification flow of the V-grade part. Budget program cost for both PROTO (verification) and V-grade (flight) devices from the start, since the anti-fuse fabric is one-time programmable and a netlist error on a flight part is unrecoverable.
Verify timing on the correct speed grade. The base RTAX2000S-CQ256PROTO is the fastest grade; if your flight bill of materials uses RTAX2000S-1CQ256PROTO or the SL -1 parts, re-run static timing analysis in Libero against the -1 timing models before committing the anti-fuse program. Timing that closes at the base grade may fail at standard grade, particularly on high fan-out clock nets near the 350 MHz class ceiling.
Design the CQFP-256 land pattern and decoupling once for both PROTO and V parts - the footprints are identical, enabling direct migration. Place low-ESR decoupling capacitors on every core and I/O bank supply pin per the RTAX-S/SL datasheet power guidelines, and use a solid ground plane under the ceramic package. For low-cost board bring-up, consider pairing with Aldec's ProASIC3E-based prototyping adaptor mapped to the CQ256 footprint to gain reprogrammability before anti-fuse commitment.
Информация о соответствии
Compliance status not published in the provided data; space-grade ceramic-packaged devices are frequently exempt from consumer RoHS scopes. Consult Microchip product compliance documentation for definitive status.
