Mars Orbiter Camera

Originally named Mars Observer Camera, it was selected by NASA in 1986 for the Mars Observer mission, but it returned only three images of planet Mars before the loss of the spacecraft in 1993. A second camera of the same specifications, renamed to Mars Orbiter Camera (MOC), was built (with assistance by California Institute of Technology) and launched on board the Mars Global Surveyor (MGS) spacecraft in 1996. The camera returned 243,668 images while in orbit around Mars, before the loss of the MGS spacecraft in 2006. Mars Orbiter Camera was operated by its manufacturer, Malin Space Science Systems, from its facilities in San Diego, California.

The scientific instrument consisted of three elements: a black-and-white narrow-angle camera with a spatial resolution of 1.4 metres per pixel (from an altitude of 378 km), and two pushbroom wide-angle cameras (one red, the other blue) with resolution capabilities spanning 230 m per pixel to 7.5 km/pixel. The narrow-angle camera provided 97,097 (roughly 40%) of the 243,668 images returned by Mars Orbiter Camera.

The narrow-angle camera was placed inside an 80 cm-long cylinder with a diameter of 40 cm, and the two wide-angle cameras were attached above the cylinder's front area. All cameras were based on CCD technology and were supported by state-of-the-art 1980s electronics, including a 32-bit radiation-hardened 10 MHz processor (capable of 1 million instructions per second) and 12 MB of DRAM memory buffer.

In addition to taking images, the MOC instrument's 12 MB memory buffer serviced the Mars Global Surveyor's Mars Relay antenna as temporary data storage for communications between Earth and landed spacecraft on Mars. For example, more than 7.6 terabits of data were transferred to and from the Mars Exploration Rovers (Spirit and Opportunity). The camera also enabled NASA scientists to choose suitable landing sites for other exploration missions.