Mars Global Surveyor
Mars Global Surveyor
Artist's conception of Mars Global Surveyor
Operator NASA Major contractors Orbiter Satellite of Mars Orbital insertion date 1997-09-12 01:17:00 UTC Launch date 1996-11-07 17:00:50 UTC
(15 years and 12 days ago)
Launch vehicle Delta 7925 Mission duration April 1, 1999 -
November 2, 2006
First extended mission
Second extended mission
Comm Relay mission
Relay extended mission
COSPAR ID 1996-062A Homepage Mars Global Surveyor Mass 1,030.5 kg (2,272 lb) Power 980 W (Solar array / 2 NiH2 batteries) Orbital elements Eccentricity .7126 Inclination 93° Apoapsis 17,836 km (11,083 mi) Periapsis 171.4 km (107 mi) Orbital period 11.64 h
The Mars Global Surveyor (MGS) was a US spacecraft developed by NASA's Jet Propulsion Laboratory and launched November 1996. It began the United States's return to Mars after a 10-year absence. It completed its primary mission in January 2001 and was in its third extended mission phase when, on 2 November 2006, the spacecraft failed to respond to messages and commands. A faint signal was detected three days later which indicated that the craft had gone into safe mode. All attempts to recontact the Mars Global Surveyor and resolve the problem failed. In January 2007 NASA officially ended the mission.
The Surveyor spacecraft, fabricated at the Lockheed Martin Astronautics plant in Denver, is a rectangular-shaped box with wing-like projections (solar panels) extending from opposite sides. When fully loaded with propellant at the time of launch, the spacecraft weighed 1,060 kg (2,337 lb). Most of Surveyor's mass lies in the box-shaped module occupying the center portion of the spacecraft. This center module is made of two smaller rectangular modules stacked on top of each other, one of which is called the equipment module and holds the spacecraft's electronics, science instruments, and the 1750A mission computer. The other module, called the propulsion module, houses Surveyor's rocket engines and propellant tanks.
- MOC - the Mars Orbiter Camera, operated by Malin Space Science Systems
- MOLA - the Mars Orbiter Laser Altimeter
- TES - the Thermal Emission Spectrometer
- MAG/ER - a Magnetometer and electron reflectometer
- USO/RS Ultrastable Oscillator for Doppler measurements
- MR Mars Relay - Signal receiver
The Mars Orbiter Camera (MOC) science investigation used 3 instruments: a narrow angle camera that took (black-and-white) high resolution images (usually 1.5 to 12 m per pixel) and red and blue wide angle pictures for context (240 m per pixel) and daily global imaging (7.5 km per pixel). MOC returned more than 240,000 images spanning portions of 4.8 Martian years, from September 1997 and November 2006. A high resolution image from MOC is either 1.5 or 3.1 km wide. So any image from this camera is at most 3.1 km wide. Often, a picture will be smaller than this because it has been cut to just show a certain feature. These high resolution images may be 3 to 10 km long. When a high resolution image is taken, a context image is taken as well. The context image shows the image footprint of the high resolution picture. Context images are typically 115.2 km square with 240 m/pixel resolution.
The Mars Relay antenna supported the Mars Exploration Rovers for data relay in conjunction with Mars Orbiter Camera's 12 MB memory buffer. In total, more than 7.6 terabits of data were transferred this way.
Launch and orbit insertion
The Surveyor spacecraft was launched from the Cape Canaveral Air Station in Florida on 7 November 1996 aboard a Delta II rocket. The spacecraft traveled nearly 750 million kilometers (466 million miles) over the course of a 300-day cruise to reach Mars on 11 September 1997.
Upon reaching Mars, Surveyor fired its main rocket engine for the 22-minute Mars orbit insertion (MOI) burn. This maneuver slowed the spacecraft and allowed the planet's gravity to capture it into orbit. Initially, Surveyor entered a highly elliptical orbit that took 45 hours to complete. The orbit had a periapsis of 262 km (163 mi) above the northern hemisphere, and an apoapsis of 54,026 km (33,570 mi) above the southern hemisphere.
After orbit insertion, Surveyor performed a series of orbit changes to lower the periapsis of its orbit into the upper fringes of the Martian atmosphere at an altitude of about 110 km (68 mi). During every atmospheric pass, the spacecraft slowed down by a slight amount because of atmospheric resistance. The density of the Martian atmosphere at such altitudes is comparatively low, allowing this procedure to be performed without damage to the spacecraft. This slowing caused the spacecraft to lose altitude on its next pass through the orbit's apoapsis. Surveyor used this aerobraking technique over a period of four months to lower the high point of its orbit from 54,000 km (33,554 mi) to altitudes near 450 km (280 mi).
On 11 October, the flight team performed a maneuver to raise the periapsis out of the atmosphere. This suspension of aerobraking was performed because air pressure from the atmosphere caused one of Surveyor's two solar panels to bend backward by a slight amount. The panel in question was slightly damaged shortly after launch in November 1996. Aerobraking was resumed on 7 November after flight team members concluded that aerobraking was safe, provided that it occurs at a more gentle pace than proposed by the original mission plan.
Under the new mission plan, aerobraking occurred with the low point of the orbit at an average altitude of 120 km (75 mi), as opposed to the original altitude of 110 km (68 mi). This slightly higher altitude resulted in a decrease of 66 percent in terms of air resistance pressure experienced by the spacecraft. During these six months, aerobraking reduced the orbit period to between 12 and 6 hours.
From May to November 1998, aerobraking was temporarily suspended to allow the orbit to drift into the proper position with respect to the Sun. Without this hiatus, 'Surveyor' would complete aerobraking with its orbit in the wrong solar orientation. In order to maximize the efficiency of the mission, these six months were devoted to collecting as much science data as possible. Data was collected between two to four times per day, at the low point of each orbit.
Finally, from November 1998 to March 1999, aerobraking continued and shrank the high point of the orbit down to 450 km (280 mi). At this altitude, Surveyor circled Mars once every two hours. Aerobraking was scheduled to terminate at the same time the orbit drifted into its proper position with respect to the Sun. In the desired orientation for mapping operations, the spacecraft always crossed the day-side equator at 14:00 (local Mars time) moving from south to north. This geometry was selected to enhance the total quality of the science return.
The spacecraft circled Mars once every 117.65 minutes at an average altitude of 378 kilometers (235 mi). It is in a near polar orbit (inclination = 93°) which is almost perfectly circular, moving from being over the south pole to being over the north pole in just under an hour. The altitude was chosen to make the orbit sun-synchronous, so that all images that were taken by the spacecraft of the same surface features on different dates were taken under identical lighting conditions. After each orbit, the spacecraft viewed the planet 28.62° to the west because Mars had rotated underneath it. In effect, it was always 14:00 for Mars Global Surveyor as it moved from one time zone to the next exactly as fast as the Sun. After seven sols and 88 orbits, the spacecraft would approximately retrace its previous path, with an offset of 59 km to the east. This ensured eventual full coverage of the entire surface.
In its extended mission, MGS did much more than study the planet directly beneath it. It commonly performed rolls and pitches to acquire images off its nadir track. The roll maneuvers, called ROTOs (Roll Only Targeting Opportunities), rolled the spacecraft left or right from its ground track to shoot images as much as 30° from nadir. It was possible for a pitch maneuver to be added to compensate for the relative motion between the spacecraft and the planet. This was called a CPROTO (Compensation Pitch Roll Targeting Opportunity), and allowed for some very high resolution imaging by the onboard MOC (Mars Orbiting Camera).
In addition to this, MGS could shoot pictures of other orbiting bodies, such as other spacecraft and the moons of Mars. In 1998 it imaged what was later called the Phobos monolith, found in MOC Image 55103.
Primary Mission Results
After analyzing hundreds of high-resolution pictures of the Martian surface taken by the orbiting Mars Surveyor spacecraft, a team of researchers found that weathering and winds on the planet create landforms, especially sand dunes, remarkably similar to those in some deserts on Earth.
Results from the Mars Global Surveyor primary mission (1996–2001) were published in the Journal of Geophysical Research by M. Malin and K. Edgett. Some of these discoveries are:
- The planet was found to have a layered crust to depths of 10 km or more. To produce the layers, large amounts of material had to be weathered, transported and deposited.
Layers in Monument Valley. These are accepted as being formed, at least in part, by water deposition. Since Mars contains similar layers, water remains as a major cause of layering on Mars.
- The northern hemisphere is probably just as cratered as the southern hemisphere, but the craters are mostly buried.
- Many features, like impact craters, were buried, then recently exhumed.
Crater that was buried in another age and is now being exposed by erosion, as seen by the Mars Global Surveyor. Image is located in the Noachis quadrangle.
- Hundreds of gullies were discovered that were formed from liquid water, possible in recent times.
Full color image of gullies on wall of Gorgonum Chaos. Image is located in the Phaethontis quadrangle.
- Large areas of Mars are covered by a mantle that coats all, but the very steepest slopes. The mantle is sometimes smooth, sometimes pitted. Some believe the pits are due to the escape of water through sublimation (ice changing directly to a vapor) of buried ice.
- Some areas are covered by hematite-rich material. The hematite could have been put in place by liquid water in the past.
- Dark streaks were found to be caused by giant dust devils. Dust Devil Tracks were observed to frequently change; some changed in just one month.
Kepler (Martian crater) showing dust devil tracks, as seen by Mars Global Surveyor. Kepler is a large crater in the Eridania quadrangle.
- The south pole's residual cap was observed to look like Swiss cheese. The holes are generally a few meters deep. The holes get bigger each year, so Mars may be warming.
- The Thermal Emission Spectrometer found that just about all of the surface of Mars is covered with volcanic rock.
Image shows both young and old lava flows from the base of Olympus Mons. The flat plain is the younger flow. The older flow has channels with levees along their edges. The presence of levees is quite common in many lava flows.
- Hundreds of house-sized boulders were found in some areas. This indicates that some materials are strong enough to hold together, even when moving downslope. Most of the boulders appeared in volcanic regions so they were probably from weathered from lava flows.
These boulders are near Ascraeus Mons, a Martian volcano. Volcanoes on Mars probably form hard boulders made up of basalt that is resistant to erosion in the current environment of Mars.
- Thousands of dark slope streaks were observed. Most scientists believe they result from the avalanching of dust. However, some researchers think that water may be involved.
Dark streaks in Diacria quadrangle, as seen by Mars Global Surveyor.
MER communications subsystem
Mars Global Surveyor functioned as a communications satellite relaying data back to Earth from the MER surface landers. Portions of MGS had been scheduled to remain active until at least September 2008 to support MER.
Loss of contact
On November 2, 2006, NASA lost contact with the spacecraft after commanding it to adjust its solar panels. Several days passed before a faint signal was received indicating that the spacecraft had entered safe mode and was awaiting further instructions.
On November 21 and 22, 2006, Mars Global Surveyor failed to relay communications to the Opportunity rover on the surface of Mars. In response to this complication, Mars Exploration Program manager Fuk Li stated, "Realistically, we have run through the most likely possibilities for re-establishing communication, and we are facing the likelihood that the amazing flow of scientific observations from Mars Global Surveyor is over."
On April 13, 2007, NASA announced the loss of the spacecraft was caused by a flaw in a parameter update to the spacecraft's system software. The spacecraft was designed to hold two identical copies of the system software for redundancy and error checking. Subsequent updating to the software encountered human error when two independent operators updated separate copies with differing parameters followed by a corrective update that unknowingly included a memory fault which resulted in the loss of the spacecraft.
- Previously, in November of 2005, two operators had changed unknowingly, the same parameter on separate copies of the system software. Each operator had used a slightly different precision when inputting a parameter, which resulted in a small but significant difference in the two copies. A subsequent memory readout revealed this inconsistency to the mission's team.
- In order to correct the error, an update was drafted in June of 2006. However, two memory addresses were incorrectly handled in the update, which could allow values to be written into the wrong memory addresses and further complications with the mission. Five months later, the problematic memory addresses were called, resulting in the solar arrays being driven until they hit a hard stop and became unmovable. The complication lead the spacecraft to incorrectly diagnose a failure of a gimbal motor causing the spacecraft to rotate to allow the unmovable solar array to point toward the Sun. However, in this position the remaining usable battery was also directed toward the Sun, resulting in the battery overheating and eventually failing. The spacecraft subsequently went into safe mode and contact with the spacecraft was lost.
Originally, the spacecraft was intended to observe Mars for 1 Martian year (approximately 2 Earth years). However, based on the vast amount of valuable science data returned, NASA had previously extended the mission three times.
MGS and general relativity: the Lense-Thirring test
Data from MGS have also been used to perform a test of the general relativistic Lense-Thirring effect which consists of a small precession of the orbital plane of a test particle moving around a central, rotating mass such as a planet. The interpretation of the out-of-plane Root-Mean-Square (RMS) time series of MGS in terms of such a relativistic feature of motion by L. Iorio was criticized by K. Krogh; however, L. Iorio supported his thesis with new arguments.
Discovery of water on Mars
On 6 December 2006 NASA released photos of two craters called Terra Sirenum and Centauri Montes which appear to show the presence of water on Mars at some point between 1999 and 2001. The pictures were produced by the Mars Global Surveyor and are quite possibly the spacecraft's final contribution to our knowledge of Mars and the question of whether life or water exists on the planet.
Hundreds of gullies were discovered that were formed from liquid water, possible in recent times. These gullies occur on steep slopes and mostly in certain bands of latitude.
- 7 November 1996: Launch from Cape Canaveral.
- 11 September 1997: Arrival at Mars, began orbit insertion.
- 1 April 1999: Primary mapping phase began.
- 1 February 2001: First extended mission phase began.
- 1 February 2002: Second extended mission phase began.
- 1 January 2003: Relay mission began.
- 30 March 2004: Surveyor photographed the Mars Exploration Rover Spirit along with its wheel tracks showing its first 85 sols of travel.
- 1 December 2004: Science and Support mission began.
- April 2005: MGS became the first spacecraft to photograph another spacecraft in orbit around a planet other than Earth when it captured two images of the Mars Odyssey spacecraft and one image of the Mars Express spacecraft.
- 1 October 2006: Extended mission phase began for another two years.
- 2 November 2006: Spacecraft suffers an error while attempting to reorient a solar panel and communication was lost.
- 5 November 2006: Weak signals were detected, indicating the spacecraft was awaiting instructions. The signal cut out later that day.
- 21 November 2006: NASA announces the spacecraft has likely finished its operating career.
- 6 December 2006: NASA releases imagery taken by MGS of a newly found gully deposit, suggesting that water still flows on Mars.
- 13 April 2007: NASA releases its Preliminary Report on the cause(s) of MGS' loss of contact. (See External Links for document)
- Exploration of Mars
- Space exploration
- Unmanned space mission
- Nickel hydrogen battery
- Phobos monolith
- "MOC Imaging Phases, Subphases, and Image Identification Numbers". http://www.msss.com/moc_gallery/moc_subphases.html. Retrieved 28 May 2006.
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- ^ [dead link]
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- ^ Malin, M. et al. 2006. Present-Day Impact Cratering Rate and Contemporary Gully Activity on Mars. science: 314. 1573-1577
- ^ "Changing Mars Gullies Hint at Recent Flowing Water". SPACE.com. 2006-12-06. http://www.space.com/scienceastronomy/061206_mars_gullies.html. Retrieved 2010-10-07.
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- NASA JPL Mars Link
- NASA mission overview
- Mars Global Surveyor Mission Profile by NASA's Solar System Exploration
- Global Surveyor Mission plan
- Malin Space Science Systems (complete image gallery)
- Preliminary Report: MGS Loss of Contact (Released 13 April 2007)
- 04/13/07: Mars Global Surveyor: Report Reveals Reasons for Loss.
- New Scientist article on the general relativistic test
- 04/13/07: Nasa confirmes first speculations about the reason for the loss of the spacecraft
- MGS Photograph
Spacecraft missions to Mars Flybys Orbiters Landers Rovers Planned missions Unplanned missions Related topics Bold italics indicate active missions ← 1995 · Orbital launches in 1996 · 1997 →STS-72 (SPARTAN-206) | PAS-3R · MEASAT-1 | Koreasat 2 | Kosmos 2327 | Gorizont #43L | Palapa C1 | N-Star B | Intelsat 708 | NEAR Shoemaker | Kosmos 2328 · Kosmos 2329 · Kosmos 2330 · Gonets-D1 #1 · Gonets-D1 #2 · Gonets-D1 #3 | Gran' #44L | Soyuz TM-23 | STS-75 (TSS-1R) | Polar | REX II | Intelsat 707 | Kosmos 2331 | IRS-P3 | STS-76 | USA-117 | Inmarsat-3 F1 | Astra 1F | MSAT-1 | Priroda | MSX | Kosmos 2332 | USA-118 | BeppoSAX | Progress M-31 | USA-119 · USA-120 · USA-121 · USA-122 · USA-123 · USA-124 | Kometa #18 | Palapa C2 · Amos-1 | MSTI-3 | STS-77 (SPARTAN-207 · IAE · PAMS-STU) | Galaxy 9 | Gorizont #44L | Cluster F1 · Cluster F2 · Cluster F3 · Cluster F4 | Intelsat 709 | STS-78 | Kobal't | TOMS-EP | USA-125 | Apstar 1A | Arabsat 2A · Turksat 1C | USA-126 | USA-127 | Progress M-32 | Télécom 2D · Italsat 2 | Molniya 1-79 | Midori · Fuji 2 | Soyuz TM-24 | Chinasat-7 | FAST | Interbol 2 · Maigon 5 · Victor | Kosmos 2333 | Kosmos 2334 · UNAMSAT-2 | Inmarsat-3 F2 | GE-1 | EchoStar II | USA-128 | STS-79 | Ekspress-6 | FSW-17 | Molniya 3-62 | HETE · SAC-B | Mars Global Surveyor | Arabsat 2B · MEASAT-2 | Mars 96 | STS-80 (WSF · ORFEUS-SPAS) | Progress M-33 | Hot Bird 2 | Mars Pathfinder (Sojourner) | Kosmos 2335 | Inmarsat-3 F3 | Kosmos 2336 | USA-129 | Bion #11 Payloads are separated by bullets ( · ), launches by pipes ( | ). Manned flights are indicated in bold text. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets.
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