RAD6000 Space Computers

Similar documents
SCS750. Super Computer for Space. Overview of Specifications

SINGLE BOARD COMPUTER FOR SPACE

A ONE CHIP HARDENED SOLUTION FOR HIGH SPEED SPACEWIRE SYSTEM IMPLEMENTATIONS

RAD750 TM SPACEWIRE-ENABLED FLIGHT COMPUTER FOR LUNAR RECONNAISSANCE ORBITER

S950 3U cpci Radiation Tolerant PowerPC SBC

GR712RC A MULTI-PROCESSOR DEVICE WITH SPACEWIRE INTERFACES

Multi-DSP/Micro-Processor Architecture (MDPA)

Development Status for JAXA Critical Parts, 2008

ATMEL SPACEWIRE PRODUCTS FAMILY

AT697E LEON2-FT Final Presentation

PowerPC- based Processor Modules for Space Applications

VORAGO TECHNOLOGIES. Rad-hard CMOS Based Technology for Space Ross Bannatyne (512)

GOES-R SpaceWire Implementation

The special radiation-hardened processors for new highly informative experiments in space

Command & Data Handling. By: Justin Hadella Brandon Gilles

Current status of SOI / MPU and ASIC development for space

System-on-a-Programmable-Chip (SOPC) Development Board

VORAGO TECHNOLOGIES. Solutions for Selective Radiation-Hardened Components in CubeSats Ross Bannatyne, VORAGO Technologies

MIL-STD-1553 (T4240/T4160/T4080) 12/8/4 2 PMC/XMC 2.0 WWDT, ETR, RTC, 4 GB DDR3

SpaceWire IP Cores for High Data Rate and Fault Tolerant Networking

Microcontrollers Applications within Thales Alenia Space products

VORAGO TECHNOLOGIES. 6 th Interplanetary CubeSat Workshop Cambridge, May, 2017

Processor and Peripheral IP Cores for Microcontrollers in Embedded Space Applications

C901 PowerPC MPC7448 3U CompactPCI SBC

High temperature / radiation hardened capable ARM Cortex -M0 microcontrollers

CNES requirements w.r.t. Next Generation General Purpose Microprocessor

Next Generation Microprocessor for Power Systems Control September 2006 M. Ruiz, SABCA, Belgium

Advanced Computing, Memory and Networking Solutions for Space

LEON3-Fault Tolerant Design Against Radiation Effects ASIC

The SpaceWire RTC: Remote Terminal Controller

Advanced Concepts and Components for adaptive Avionics

1. Microprocessor Architectures. 1.1 Intel 1.2 Motorola

16th Microelectronics Workshop Oct 22-24, 2003 (MEWS-16) Tsukuba Space Center JAXA

VORAGO TECHNOLOGIES. Radiation-Hardened Solutions for CubeSats Ross Bannatyne, VORAGO Technologies

HIGH PERFORMANCE PPC BASED DPU WITH SPACEWIRE RMAP PORT

ARM-Based Embedded Processor Device Overview

The High-Reliability Programmable Logic Leader. Products for Space Applications. QML Certification Part of Overall Quality Platform

HXRHPPC Processor Rad Hard Microprocessor

C900 PowerPC G4+ Rugged 3U CompactPCI SBC

Intelop. *As new IP blocks become available, please contact the factory for the latest updated info.

Rad-Hard Microcontroller For Space Applications

Space: The Final Frontier FPGAs for Space and Harsh Environments

Scalable Sensor Data Processor Development Status DSP Day - September 2014

MIL-STD-1553 (T4240/T4160/T4080) 12/8/4 2 PMC/XMC 2.0 WWDT, ETR, RTC, 4 GB DDR3

ADVANCED ELECTRONIC SOLUTIONS AVIATION SERVICES COMMUNICATIONS AND CONNECTIVITY MISSION SYSTEMS

FPGAs for Space Applications

VMEbus 16 port Asynchronous Communications Multiplexer MVC EOL Notice

IMPLICIT+EXPLICIT Architecture

Space Micro Satellite Computer Goals Space Computer Performance Goals: >1,000 MIPS throughput Less than 1 SEU in 1,000 days Less than 10 watts power R

The Nios II Family of Configurable Soft-core Processors

MultiChipSat: an Innovative Spacecraft Bus Architecture. Alvar Saenz-Otero

Programming Environments Manual For 32 Bit Implementations Of The Powerpc Architecture

DEVELOPING RTEMS SMP FOR LEON3/LEON4 MULTI-PROCESSOR DEVICES. Flight Software Workshop /12/2013

FPGAs in radiation-harsh environments

SCP/DCP U cpci Single Board Computer. Features P R O D U C T D ATA S H E E T

Nitro240/260 CPU Board Scalable 680x0 VME board for I/O intensive applications

Memory Expansion. Lecture Embedded Systems

Atmel s s AT94K Series Field Programmable System Level Integrated Circuit (FPSLIC)

About using FPGAs in radiation environments

Next Generation Multi-Purpose Microprocessor

Sun Fire V880 System Architecture. Sun Microsystems Product & Technology Group SE

Your Company Logo Here. Flying High-Performance FPGAs on Satellites: Two Case Studies

ZT 5520 CPU BOARD WITH SINGLE/DUAL PENTIUM PRO PROCESSORS

FPGAs APPLICATIONS. 2012, Sept Copyright Atmel Corporation

Computer Maintenance. Unit Subtitle: Motherboards. Copyright Texas Education Agency, All rights reserved. 1

A171 Rugged Compact PC

SpaceWire Remote Terminal Controller

ESA Contract 18533/04/NL/JD

SpaceWire 101. Webex Seminar. February 15th, 2006

AMC data sheet. PMC Module with four CAN bus Nodes ARINC825 compliant for Testing & Simulation of Avionic CAN bus Systems

EPC -8 Highly integrated Intel486 -based VMEbus Embedded CPU

VXS-610 Dual FPGA and PowerPC VXS Multiprocessor

Military Grade SmartFusion Customizable System-on-Chip (csoc)

A Novel Approach to a High Speed, Large Memory Spacecraft Data Storage Unit

C800 Core 2 Duo CompactPCI SBC

Xilinx Virtex-5QV Update and Space Roadmap Kangsen Huey Space Marketing Aerospace & Defense 17th, March, 2016

VMICPCI-7755 Intel Pentium III Processor-Based CompactPCI System Controller SBC with 133 MHz System Bus

MIPS R4300I Microprocessor. Technical Backgrounder-Preliminary

C802 Core i7 3U CompactPCI SBC

Transputers. The Lost Architecture. Bryan T. Meyers. December 8, Bryan T. Meyers Transputers December 8, / 27

Artisan Technology Group is your source for quality new and certified-used/pre-owned equipment

A Reference Architecture for Payload Reusable Software (RAPRS)

Artisan Technology Group is your source for quality new and certified-used/pre-owned equipment

RAD55xx Platform SoC. Dean Saridakis, Richard Berger, Joseph Marshall *** *** *** *** *** *** *** photo courtesy of NASA

StrongARM** SA-110/21285 Evaluation Board

Artisan Technology Group is your source for quality new and certified-used/pre-owned equipment

79C Megabit (512K x 40-Bit) EEPROM MCM FEATURES: DESCRIPTION: Logic Diagram. 512k x 40-bit EEPROM MCM

Systems in Silicon. Converting Élan SC400/410 Design to Élan SC520

386EX PC/104 Computer with CompactFlash and PCMCIA SBC1390

A12C - 6U VMEbus MPC8245 SBC / PMC

Configurable Fault Tolerant Processor (CFTP) for Space Based Applications

ADM-96S AND ADM-48D HIGH PERFORMANCE DATA ACQUISITION SYSTEMS

CPCI-6020 CompactPCI Host Slot Processor Board

Recent ASIC Developments by NEC

Embedded Systems: Architecture

Memory hierarchy and cache

1 COMMAND AND DATA HANDLING (C&DH)

A brief History of INTEL and Motorola Microprocessors Part 1

ASICs Digital and Mixed-Signal

L2: FPGA HARDWARE : ADVANCED DIGITAL DESIGN PROJECT FALL 2015 BRANDON LUCIA

Transcription:

RAD6000 Space Computers

RAD6000 space computers RAD6000 single-board computers combine commercial standards with unique radiation-hardened technology and packaging to meet the specific requirements of space applications. The RAD6000 computers include support functions to control local memory and provide standard and custom I/O interfaces. Support functions are implemented in both FPGAs and ASICs. The FPGA versions are based on the popular VME standard interface. The ASIC version supports multiple I/O devices and protocols and uses PCI as the common, on-card bus interface. This feature ensures a seamless software transition to the higher-performance RAD750 TM computer, also based on PCI. BAE Systems has consolidated its space programs into the Space Systems and Electronics (SS&E) organization. Performing organizations are located in Nashua and Merrimack, New Hampshire; Manassas, Virginia; and Colorado Springs, Colorado. Today, BAE Systems develops and produces a wide array of space mission solutions from single-board radiation-hardened computers to complete space payloads. SS&E in Manassas, Virginia continues to specialize in radiation-hardened electronics and space applications including ASICs, memories, and single-board computers. Today, SS&E has more than 400 computers in space, including the RAD750, the RAD6000 (32-bit), and the GVSC 1750 (16-bit). The first RAD750s, the next-generation space computer, were launched in 2005.

RAD6000 microprocessor The RAD6000 is a low-cost, high-performance 32-bit Reduced Instruction Set Computer (RISC). The RAD6000 combines the popular and proven Power Architecture of the IBM RISC System/6000 workstation with BAE Systems QML qualified, radiation-hardened CMOS process to provide powerful and flexible solutions for space applications. SEU hardening has been applied to all storage elements in the RAD6000 including latches, registers, and RAMs. RAD6000 key features Up to 35 Dhrystone 2.1 MIPS at 33 MHz Radiation-hardened 32-bit RISC super scalar single chip CPU 8 KByte internal cache Low-power 3.3 volt operation 72-bit (64 data, 8 ECC) memory bus Variable power/performance Independent fixed and floating point units with concurrent operation Temperature range -25 C to +105 C Radiation-hardness levels Total dose: > 1 Mrad (Si) Latchup: Immune SEU: 7.4E-10 errors/bit-day (90% W.C. GEO) RAD6000 Microprocessor

RAD6000 radiation-hardened processor product family The versatility of the RAD6000 is demonstrated in the variety of past and current application configurations available, including packaging options, architecture variations, memory configurations, and I/O selections. Being gate-for-gate identical with its commercial counterpart, the RAD6000 uses many commercial software products without modification, including the industry-leading Vx-Works TM operating system, significantly reducing application software development costs and risk. Mars Rover RAD6000 flight computer, FPGA-based Of course there is intelligent life on Mars... we helped put it there!

Processor board configuration information (other configurations available) ASIC-Based Single Board Computers CompactPCI FPGA-Based Dual/Triple Redundant Computer Subsystem Performance Variable to 35 MIPS Variable to 26 MIPS Variable to 22 MIPS Variable to 21 MIPS per processor Frequency Variable to 33 MHz Variable to 25 MHz Variable to 20 MHz Variable to 20 MHz Power (maximum) < 10 Watts at 33 MHz < 7.5 Watts at 25 MHz 20 Watts at 20 MHz 11.9 Watts (EOL) at 20 MHz per processor Power (low) 2.5 Watts at 4.1 MHz < 3.1 Watts at 5 MHz 5 Watts at 2.5 MHz 8 Watts (EOL) at 2.5 MHz per processor Memory 8 MByte SRAM 8 or 16 MByte SRAM 128 MByte DRAM 4 MByte SRAM EEPROM/PROM Up to 128 Kbyte PROM 4 MByte EEPROM 3 MByte EEPROM EEPROM configurable 1, 2, 3, 4 MByte 128 Kbyte PROM Mass (board) < 1.0 Kg < 0.9 Kg < 1.2 Kg < 4.8 Kg (2 processors and power supplies in box) Size IEEE 1101.7 (6 9 ) 6U Compact PCI 6U VME 10.3 2.9 8 excluding mounting feet Interfaces ASCM module bus, RS422 1553, UART, PCI, discretes, interrupts RS232 Support functions ASIC ASIC FPGA ASIC & FPGA 1553, serial UART, discretes in & out, interrupts RAD6000 architecture COP bus RS-422 Software developed for RAD6000 is upwardly compatible to RAD750 RAD6000 CPU LIO bridge System memory UART Port JTAG RAD750 TM CPU Power PCI bridge System memory PCI bus JTAG bus PCI bus JTAG bus AMBI QHSS PLASMA TM bus ASCM module bus 1553 Serial channels IEEE 1394 firewire

Variety of standard interfaces supported ASCM module bus MIL-STD 1553 High-Speed Serial (HSS) IEEE 1394 backpanel I/F PCI (via LIO chip) RS-422 or RS-232 UART RAD6000 ASIC-based single board computer Dual/triple redundant computer subsystem with power supply

www.pcfly.info For further information, contact: BAE SYSTEMS 9300 Wellington Road Manassas, VA 20110-4122 Telephone 1-866-530-8104 www.baesystems.com/sse Cleared for Open Publication by DoD 07/06 2006 BAE SYSTEMS CompactPCI is a registered trademark of the PCI Industrial Manufacturers Group. RISC systems ia a registered trademark of IBM. The PowerPC name, PowerPC 750, and the PowerPC logotype are trademarks of International Business Machines Corp., used under license therefrom. VxWorks is a registered trademark of Wind River Systems PUBS-06-A49