IBM RAD6000

The radiation-hardening of the original RSC 1.1 million-transistor processor to make the RAD6000's CPU was done by IBM Federal Systems Division working with the Air Force Research Laboratory.

As of June 2008, there are 200 RAD6000 processors in space on a variety of NASA, United States Department of Defense and commercial spacecraft, including:

• Mars Exploration Rovers (Spirit and Opportunity)
• Deep Space 1 probe
• Mars Polar Lander and Mars Climate Orbiter
• Mars Odyssey orbiter
• Spitzer Infrared Telescope Facility
• MESSENGER probe to Mercury
• STEREO Spacecraft
• IMAGE/Explorer 78 MIDEX spacecraft
• Genesis and Stardust sample return missions
• Phoenix Mars Polar Lander
• Dawn Mission to the asteroid belt using ion propulsion
• Solar Dynamics Observatory, Launched Feb 11, 2010 (flying both RAD6000 and RAD750)[1]
• Burst Alert Telescope Image Processor on board the Swift Gamma-Ray Burst Mission
• DSCOVR Deep Space Climate Observatory spacecraft

The computer has a maximum clock rate of 33 MHz and a processing speed of about 35 MIPS.[2] In addition to the CPU itself, the RAD6000 has 128 MB of ECC RAM.[2] A typical real-time operating system running on NASA's RAD6000 installations is VxWorks. The Flight boards in the above systems have switchable clock rates of 2.5, 5, 10, or 20 MHz.

Reported to have a unit cost somewhere between US$200,000 and US$300,000, RAD6000 computers were released for sale in the general commercial market in 1996.

The RAD6000's successor is the RAD750 processor, based on IBM's PowerPC 750.

• IBM RS/6000
• PowerPC 601, a consumer chip with similar computing capabilities to the RAD6000

• Software on Mars rovers 'space qualified' – By Matthew Fordahl/AP, 23 January 2004
• AFRL Rad6000 fact sheet
• Software Behind the Mars Phoenix Lander (Audio Interview)
• The CPUs of Spacecraft Computers in Space