Mars Global Surveyor entered a 258 x 54021 km x 93.3 deg polar orbit around Mars on 12 September 1997 after a 22 minute burn of its main engine. After aerobraking ended in February 1999, MGS was in a 118 minute circular polar science mapping orbit with an index altitude of 378 km. Because of the high volume of data which imaging experiments can generate, the MOC electronics contain not only a large amount of memory (~12 MB DRAM buffer) for processing and storing the images, but also have the capability of utilizing a number of data compression techniques (both lossless and lossy). Four solar array panels (2 GaAs, 2 SI) provide 980 W of power to the spacecraft.

All instruments except the magnetometer are stored on the nadir equipment deck, on one of the 1.17 x 1.17 meter surfaces. Radio Science (Ultrastable Oscillator) to study gravitational field, atmospheric refractive indices, and temperature profiles. The electronics for the MOC are completely redundant and the narrow-angle and wide-angle cameras can be operated by either set of electronics and all three cameras can be operated simultaneously.

The wide-angle assembly consists of two cameras mounted on the side of the narrow-angle assembly.

Mars Global Surveyor was the first spacecraft in NASA’s new Mars Surveyor Program, a new generation of American space probes to explore Mars every 26 months from 1996 to 2005. However, one of the solar panels failed to latch properly when it was deployed and subsequently showed unexpected motion and moved past its fully deployed position when aerobraking began (thought to be due to the fracture of a damper arm and subsequent structural damage).

NASA NSSDC Master Catalog Description. These two assemblies are contained within a single cylindrical structure, approximately 80 cm in length and 40 cm in diameter.

Over the next four months, it was intended that aerobraking maneuvers and thrusters would be used to lower the orbit to the final circular mapping orbit. After each orbit, the spacecraft viewed th…
After the initial elliptical capture orbit, months of thruster firings and aerobraking maneuvers were used to reach the nearly circular mapping orbit. As a result, the equivalent of two, four, or eight (depending on mission phase) 2048 x 2048 pixel images can be processed on record-only days and, once every three days on average, fourteen such images can be processed and sent during an eight-hour real-time pass. Mars Orbiter Camera (MOC) supported study of climate, surface geology, and surface and atmospheric interactions. Science observations were made periodically during these maneuvers. Power System: 4 Solar Array Panels, 667 W. The Mars Global Surveyor (MGS) mission is designed as a rapid, low-cost recovery of the Mars Observer mission objectives. Further, the MOC can transfer these data (either to the on-board recording system or via real-time transmission) at any rate of which the spacecraft is capable. One wide-angle camera, optimized to operate in a band pass from 400-450 nm (``blue'') has a focal length of 11.4 mm (f/6.3). Mars Global Surveyor was the first successful U.S. mission launched to Mars since the Viking mission in 1976.

Its primary objectives are to: (1) obtain global, synoptic views of the Martian surface and atmosphere on a daily basis in order to understand the meteorological and climatological changes during the mission; (2) monitor surface and atmospheric features for changes on temporal scales from hours to years and on a spatial scale necessary for resolving the details of their morphology; and, (3) systematically examine local areas at high spatial resolution so that surface/atmosphere interactions and geologic processes which operate on short time scales can be quantified. The main 596 N thruster wil use hydrazine and N2O4 propellant.

Two solar panels, each 3.5 x 1.9 m in size, extend out from opposite sides of the craft.

See just a few highlights from the spacecraft that has orbited Mars for nearly ten years.

The spacecraft went silent after an incorrect software upload caused its solar arrays to lose power. Energy is stored in two 20 Amp-hr nickel hydrogen batteries, and supplied at 28 V DC. › Slide Show: Mars Global Surveyor › View Archive In order to acquire images to satisfy these three objectives, the MOC consists of a narrow-angle assembly and a wide-angle assembly. Images that provide evidence of recent water flows on Mars.

The spacecraft itself is a rectangular box approximately 1.17 x 1.17 x 1.7 meters in size, made up of two parts, the equipment module and the propulsion module.

Some opportunities for in-flight calibration are possible during regional or global dust storms.

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