OPF S1 Working Group · Heritage Reference · OpenPOWER Foundation

The Processors That Reached
Mars, Jupiter, and the Stars

BAE Systems RAD750 and RAD6000 POWER processors flew on Mars Curiosity, Perseverance, the James Webb Space Telescope, and over 200 other space missions. We're open-sourcing this radiation-hardened silicon heritage and making it available for the next generation of spacecraft.

Mars Curiosity Rover Mars Perseverance Rover James Webb Space Telescope Mars Reconnaissance Orbiter Deep Space 1 Orion Spacecraft
Explore the Chip Families Join the Initiative
200+
Space missions flown on POWER architecture processors
RAD750
The Mars rover brain — Curiosity and Perseverance, still operating
JWST
James Webb Space Telescope — RAD750 on the most complex observatory ever built
25+ yr
RAD6000 operational in deep space — Spirit still sending data after 15 years
The Heritage Chip Families

The POWER Processors That Flew to Space

BAE Systems and Freescale built successive generations of radiation-hardened POWER processors for space applications. Each generation was tested to survive the Van Allen belts, deep space cosmic rays, solar particle events, and the extreme temperature cycling of low Earth orbit — then validated in actual missions before being certified for crewed flight.

1998
RAD6000
Deep Space 1 — first flight
2003
RAD6000
Mars Spirit & Opportunity
2006
RAD750
Mars Reconnaissance Orbiter
2011
RAD750
Curiosity Rover launch
2021
RAD750
JWST + Perseverance Rover
Generation 1 · 1997–2006

BAE Systems RAD6000

Radiation-hardened POWER1 ISA · 33 MHz · 12 MIPS
CPU Core
POWER1 ISA (RS/6000)
Max Clock
33–200 MHz (versions)
Rad Hardness
300 krad(Si) TID
Process
250 nm rad-hard CMOS

The RAD6000 was derived from the IBM RS/6000 workstation processor and radiation-hardened by BAE Systems (then Loral Federal Systems). Its silicon-on-insulator process and radiation-hardened cell library gave it immunity to single-event upsets that would corrupt conventional SRAM and flip-flops. The RAD6000 flew on Mars Pathfinder (1997), Mars Spirit and Opportunity (2004), and over 150 other missions. Spirit operated on Mars for over 6 years — well beyond its 90-day design lifetime — with the RAD6000 performing flawlessly throughout.

Mars Pathfinder Spirit Rover Opportunity Rover Deep Space 1 150+ Missions
Open-source initiative — in scoping
Generation 2 · 2001–present

BAE Systems RAD750

Radiation-hardened PowerPC 750 (G3) · 200 MHz · 400 MIPS
CPU Core
PowerPC 750 (G3)
Max Clock
200 MHz
Rad Hardness
1 Mrad(Si) TID
Process
150 nm rad-hard CMOS

The RAD750 is the successor to the RAD6000 and the most widely-flown space processor in history. Based on the PowerPC G3 (Apple's iMac CPU), radiation-hardened by BAE Systems through a combination of silicon-on-insulator fabrication, radiation-hardened flip-flops, and triple-module redundancy in critical paths. It delivers 400 MIPS at 200 MHz while surviving 1 Mrad of total ionizing dose. The RAD750 currently controls Mars Curiosity and Perseverance — both rovers are still actively operating — as well as the James Webb Space Telescope, which carries two RAD750s for redundancy. Approximately 200+ RAD750 units have been delivered for flight missions.

Mars Curiosity (2012–) Mars Perseverance (2021–) JWST (2021–) Mars Recon. Orbiter LRO
Open-source initiative — in scoping
Generation 3 · 2010s

BAE Systems RAD5500

Radiation-hardened PowerPC 750FX enhanced · 400 MHz
CPU Core
PowerPC 750FX enhanced
Max Clock
400 MHz
Rad Hardness
>1 Mrad(Si) TID
Process
90 nm rad-hard

The RAD5500 doubles the clock rate of the RAD750 with an enhanced 750FX pipeline and improved memory interface. Targeting next-generation deep space and interplanetary missions where the computational demands of autonomous navigation and science payload processing exceed what the RAD750 can deliver. The PowerPC 750FX core also flew in the Orion spacecraft (NASA Exploration Flight Test-1) on non-rad-hard versions before the full RAD5500 was available, demonstrating the POWER ISA's suitability for crewed spaceflight.

NASA Next-Gen Deep Space Orion (750FX-derived) ESA Science Missions
Open-source initiative — in scoping
Commercial Space · 2010s

Freescale e500 / Space Micro Proton

P2020 / e500mc · Proton 400k · Commercial space applications
CPU Core
e500 / e500mc
Max Clock
1.2–1.5 GHz
Rad Hardness
50–100 krad (product-dependent)
Process
45 nm (COTS enhanced)

Space Micro's Proton 400k integrates a commercial Freescale P2020 QorIQ processor (dual e500mc POWER cores) with radiation-mitigation techniques including EDAC-protected memories, watchdog recovery, and selective triple-module redundancy — delivering space-qualification at commercial cost. TESS (Transiting Exoplanet Survey Satellite) flew a Space Micro board with POWER e500 cores for its science data processing computer, demonstrating that commercial POWER silicon with appropriate mitigation can serve real space missions at dramatically lower cost than full rad-hard ASICs.

TESS (NASA, 2018–) Commercial LEO Missions CubeSat / SmallSat
Open-source initiative — in scoping

Radiation Hardening: Why POWER Survived Where Others Failed

Space radiation causes two classes of failures: Total Ionizing Dose (TID) — cumulative radiation degrading transistor characteristics over years — and Single Event Effects (SEE) — cosmic ray strikes that flip individual bits or latch up circuit states. The RAD6000 and RAD750 address both: silicon-on-insulator (SOI) fabrication eliminates latch-up entirely, radiation-hardened flip-flops are immune to single-bit upsets, and the POWER ISA's software-managed cache (no hardware speculative state that needs protecting) simplifies recovery. The result is processors that have operated for 25+ years in deep space — far beyond any design lifetime — with zero SEE-induced failures.

1 Mrad
Total Ionizing Dose tolerance (RAD750)
SEU-immune
Single Event Upsets — rad-hard flip-flops eliminate bit flips
SOI
Silicon-On-Insulator — eliminates latch-up failure mode entirely
25+ yr
Demonstrated operational life in deep space beyond design lifetime
200+
Space missions on POWER architecture
1 Mrad
RAD750 total ionizing dose tolerance
JWST
Most complex space observatory ever built — runs POWER
3 Gen
RAD6000 → RAD750 → RAD5500 / e500
Mission Record

From Mars to the Edge of the Solar System

POWER processors didn't just fly in space — they executed the science, navigation, and autonomy algorithms that made these missions successful. When the Perseverance rover drives itself across Mars, it's POWER ISA instructions making every decision.

Mars Surface

Curiosity & Perseverance Rovers

Both active Mars rovers run RAD750 processors at 200 MHz. Curiosity has operated since August 2012 — over 4,500 Martian days. Perseverance landed in February 2021 and has collected the first samples intended for eventual return to Earth. The POWER core executes autonomous navigation, science target selection, and hazard avoidance algorithms.

Space Telescope

James Webb Space Telescope

JWST carries two RAD750 processors — one primary, one backup — that coordinate the 18-segment gold mirror, fine guidance sensor, and all four science instruments. The telescope operates at L2, 1.5 million km from Earth, where servicing is impossible. POWER ISA reliability was a primary selection criterion.

Mars Orbit

Mars Reconnaissance Orbiter

MRO launched in 2005 and has been in continuous Mars orbit since 2006. Its RAD750 controls the HiRISE camera (the highest-resolution camera ever sent to another planet), CRISM spectrometer, and communications relay for surface missions. Still operational after 20 years.

Pioneer

Deep Space 1 (RAD6000)

The first spacecraft to use the RAD6000 for primary mission computing, Deep Space 1 validated ion propulsion and 12 other advanced technologies in 1998-2001. It flew within 2,200 km of Comet Borrelly — the closest cometary flyby in history at the time — with POWER ISA processors executing its autonomous navigation.

Mars Surface

Spirit & Opportunity (RAD6000)

Spirit operated for 6.2 years (90-day design life). Opportunity operated for 14.5 years — the longest operational Mars surface mission in history. Both ran RAD6000 processors. The POWER ISA executed every drive command, instrument reading, and uplink/downlink session across the entire operational lifetime.

Commercial Space

TESS Exoplanet Survey (e500)

NASA's TESS satellite, launched in 2018, uses Space Micro's Proton 400k board with Freescale POWER e500mc cores for science data processing. TESS has discovered thousands of exoplanet candidates — its science computer runs POWER ISA at roughly 100× the computational performance of the RAD750 at lower cost.

Why Open Source It

The Case for Open Space-Grade Silicon

The space processor market is a near-monopoly. BAE Systems RAD750/5500 and the Microchip LEON family account for the overwhelming majority of deep-space processors. An open-source POWER space core breaks this dependency — and enables a generation of national space programs and commercial missions to build on proven heritage.

25 Years of Flight Heritage

The RAD750 architecture has been validated in 200+ actual space missions across the entire solar system. No simulation or ground test can replicate this. An open-source implementation inherits the credibility of that mission record.

Sovereign Space Computing

Nations building sovereign space programs — India, Brazil, South Korea, UAE — need access to space-grade processors without US ITAR export controls. An open POWER ISA space core, fabricated domestically, removes this dependency entirely.

Commercial Space Cost Reduction

RAD750 units cost $200,000–$500,000 each. An open-source POWER space core can be fabricated in radiation-tolerant processes at a fraction of that cost — enabling CubeSat and SmallSat missions that can't afford traditional rad-hard ASICs.

POWER ISA 3.1 for Autonomous Space AI

Next-generation autonomous spacecraft need more computation for onboard science processing, navigation AI, and real-time instrument response. POWER ISA 3.1 MMA extensions enable neural network inference directly on a flight processor — without a separate GPU or NPU.

Open Radiation Characterization

Radiation testing data for POWER cores exists across decades of NASA and ESA programs. An open-source implementation enables open radiation test campaigns — sharing single-event effect data across the entire community rather than locking it in vendor NDAs.

ISA Continuity Across Space Generations

Software written for RAD6000 (1997) runs on RAD750 (2001) runs on modern POWER servers. This ISA continuity means mission software developed for open POWER space cores will remain compatible as the hardware scales — a critical advantage for 10+ year mission lifetimes.

Verify with IBM EDA Suite via Silicon Factory

IBM SixthSense · EINSTEIN · BooleDozer — radiation analysis and tape-out flows via the OpenPOWER Silicon Factory.
OPF S1 Working Group · Development Path

Heritage In → OPF S1 Out

These space cores are the reference material — not the final product. The OPF S1 Working Group consolidates the RAD750, RAD6000, and e500 space heritage into a single unified OPF S1 radiation-tolerant core. It then goes through POWER ISA 3.1 update with MMA for autonomous onboard science processing, AI-assisted EDA verification with radiation-corner timing analysis, and tape-out at Intel Foundry, Samsung, or TSMC using radiation-tolerant process variants at 7/5nm.

Phase 1 — Open Source RTL

Release the Space Core RTL

Work with BAE Systems, NASA, and the POWER ISA community to release synthesisable Verilog implementations of the PowerPC 750 core — the architectural foundation of the RAD750 — under an open license, with radiation-hardening documentation.

  • Coordinate IP release with BAE Systems and heritage holders
  • Publish PowerPC 750 core RTL to GitHub under OpenPOWER Foundation
  • Document rad-hard cell requirements, TMR topology, and ECC implementation
  • Include VxWorks and RTEMS BSP test infrastructure
  • Provide NASA GSFC flight software interface documentation
Phase 2 — POWER ISA 3.1 Update

Modernize to Current ISA

Update the PowerPC 750 core to implement POWER ISA 3.1, adding MMA extensions for onboard AI/science processing, a 64-bit capable ABI, and improved cache/prefetch — while preserving full compatibility with existing space flight software stacks.

  • Implement POWER ISA 3.1 base instruction set
  • Add Matrix Math Assist (MMA) for autonomous science and ADAS-in-space
  • Maintain backward compatibility with RAD6000/RAD750 flight software
  • Update RTEMS and VxWorks BSPs for new ISA features
  • Radiation analysis of new pipeline stages under proton and heavy ion bombardment models
Phase 3 — EDA Verify + Tape Out

Silicon Verification and Tape-Out

Run the updated space core through complete EDA flows — formal verification, radiation-corner timing analysis, and single-event effects simulation — then tape out in a radiation-tolerant process suitable for space missions.

  • JasperGold / VC Formal for TMR redundancy correctness proofs
  • Tempus / PrimeTime timing at radiation-degraded corner (end-of-life transistor parameters)
  • Voltus / RedHawk power analysis for solar panel power budget compatibility
  • Target radiation-tolerant process (SkyWater 130T or equivalent open PDK)
  • Single Event Upset rate simulation using CREME96 / MUSCAT models
  • NASA Technology Readiness Level (TRL) advancement documentation

Join the Space Heritage Cores Initiative

Whether you're a national space agency, a commercial satellite operator, a university CubeSat program, or a sovereign space initiative, POWER's space heritage offers a path to open, proven, radiation-tolerant silicon. Let's fly together.

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