MARCI consists of nadir-pointed wide angle and medium angle cameras. Each camera has its own unique optics and identical focal plane assemblies, data acquisition system electronics, and power supplies. MARCI is mounted on the bottom (nadir pointing side) of the spacecraft. Each camera consists of a stray light baffle and lens elements and filters which focus onto an electronically-shuttered CCD. Without the baffle, the wide-angle camera is approximately 4.8 x 4.8 x 3.8 cm and the medium angle camera 5.4 x 5.4 x 5.5 cm. The wide-angle baffle extends an additional 1.4 cm and the medium angle baffle 2 cm. The cameras operate in push-frame fashion, in which a filter plate, consisting of multiple narrowband filter strips in the cross-track direction, is mounted over the detector. Consecutive images are taken each time the camera footprint advances one filter-width (about 20 pixels) in the downtrack direction. The images are 1000 x 1000 pixels in size. The MARCI operating temperature range is -40 to +70 degrees C and survival range is -80 to +100 degrees C.5
The wide-angle camera has a field of view of 140 degrees. It has a dual lens system consisting of a five-element fused silica f/6 lens for short UV and a seven-element optical glass f/5 lens for longer UV and visible light. The optical paths of both lens systems are combined by a prism and dichroic beamsplitter, giving an effective focal length of 4.3 mm. It is capable of obtaining images in 7 spectral bands, 5 visible and 2 UV at a resolution of 7.2 km/pixel or better. The raw data rate from the wide-angle camera is 29.6 kbps per band.6
The medium-angle camera has a field-of-view of 6 degrees. It has an f/2 catadioptric lens consisting of six elements, five of SiO2 and one of BK7, with an effective focal length of 87.9 mm. Images can be obtained in any of 10 spectral bands, ranging from 425 to 1000 nm, at a nadir resolution of 40 m/pixel. The raw data rate from the medium-angle camera is 704 kbps per band.7
Under proper conditions, resolutions up to 1 kilometer (3300 ft) are possible.89 The principal investigator on this project was Michael Malin at Malin Space Science Systems and the project was reincorporated on Mars Reconnaissance Orbiter. Its objectives:10
"Spacecraft Parts: Instruments: MARCI". MARCI website. Archived from the original on May 5, 2006. Retrieved June 2, 2006. https://web.archive.org/web/20060505023016/http://www.msss.com/mro/marci/description.html ↩
"Mars Color Imager: How MARCI Takes Color Images, MRO MARCI Release No. MARCI2-3, 13 April 2006". Archived from the original on May 13, 2013. Retrieved March 13, 2012. http://www.msss.com/mro/marci/images/2006/04/13/marci_detail/index.html ↩
"NASA - NSSDCA - Experiment - Details". nssdc.gsfc.nasa.gov. Retrieved 2 February 2023. This article incorporates text from this source, which is in the public domain. https://nssdc.gsfc.nasa.gov/nmc/experiment/display.action?id=1998-073A-01 ↩
"MARS RECONNAISSANCE ORBITER (MRO) MARS COLOR IMAGER (MARCI) INSTRUMENT DESCRIPTION". msss.com. Malin Space Science Systems. Retrieved 2 February 2023. https://www.msss.com/science/mro-marci-instrument-description.php ↩
Malin, M.C.; Bell (III), J.F.; Calvin, W.M.; Caplinger, M.A.; Clancy, R.T.; Harberle, R.M.; James, P.B.; Lee, S.W.; Ravine, M.A.; Thomas, P.; Wolff, M.J. (2001). "Mars Color Imager (MARCI) on the Mars Climate Orbiter" (PDF). Journal of Geophysical Research. 106 (E8): 17, 651–17, 672. Bibcode:2001JGR...10617651M. doi:10.1029/1999JE001145. Retrieved January 13, 2011. http://www.msss.com/mro/marci/references/1999JE001145.pdf ↩
"Mars Color Imager (MARCI)". NASA / National Space Science Data Center. Retrieved February 19, 2011. https://nssdc.gsfc.nasa.gov/nmc/experiment/display.action?id=1998-073A-01 ↩