| Mars Science Laboratory | |
2007 Mars Science Laboratory concept | |
| Organization | NASA |
|---|---|
| Mission type | Rover |
| Orbital insertion date | July-September 2010 |
| Webpage | MSL Home Page |
The Mars Science Laboratory (or MSL for short) is a NASA rover scheduled to launch in September 2009 and perform a precision landing on Mars in July-September 2010. The National Aeronautics and Space Administration ( NASA, ˈnæsə is an agency of the United States government, responsible for the nation's public space program A rover is a Space exploration vehicle designed to move across the surface of a Planet or other Astronomical body. This rover will be three times as heavy and twice the width of the Mars Exploration Rovers (MERs) that landed in 2004. NASA 's Mars Exploration Rover ( MER) Mission is an ongoing robotic mission of exploring Mars, that began in 2003 with the sending of It will carry more advanced scientific instruments than any other mission to Mars to date, including analysis of samples scooped up from the soil and drilled powders from rocks. Soil, often typeset as SOiL, is a four piece rock band from Chicago Illinois United States founded by Shaun Glass Tom Schofield Tim King and Adam Zadel In Geology, rock is a naturally occurring aggregate of Minerals and/or Mineraloids The Earth's outer solid layer the ‘ Lithosphere It will also investigate the past or present ability of Mars to support life. Life is a state that distinguishes Organisms from non-living objects such as non-life and dead organisms being manifested by growth through Metabolism The international community will provide some of the instruments onboard.
The MSL rover will be launched by an Atlas V 541. The Atlas V Rocket is an Expendable launch vehicle formerly built by Lockheed Martin and now built by the Lockheed Martin- Boeing joint venture MSL will be expected to operate for at least 1 martian year (668 sols) as it explores with greater range than any previous Mars rover. Various schemes have been used or proposed to keep track of time and date on the planet Mars independently of Earth time and calendars Solar times are measures of the apparent position of the Sun on the Celestial sphere.
In September 2006, MSL was approved by NASA HQ for a 2009 launch. Several JPL engineers working on MSL have informally stated that the MSL design will likely be used on future rovers after the first MSL is launched in 2009.
In April 2008, USA Today reported that the project is $235 million, or 24%, over budget. USA TODAY is a national American daily Newspaper published by the Gannett Company. The money to compensate this overrun should come from other NASA Mars missions, meaning a significant cut. [1]
MSL is expected to weigh over 800 kg (1,760 lb) including 65 kg (143 lb) of scientific instruments, compared to the Mars Exploration Rovers which weigh 185 kg (407 lb) including 5 kg (11 lb) of scientific instruments. The pound or pound-mass (abbreviation lb, lbm, or sometimes in the United States #) is a unit of Mass NASA 's Mars Exploration Rover ( MER) Mission is an ongoing robotic mission of exploring Mars, that began in 2003 with the sending of MSL will be able to roll over obstacles approaching 75 cm (29 in) in height. A centimetre ( American spelling: centimeter, symbol cm) is a unit of Length in the Metric system, equal to one hundredth Maximum terrain-traverse speed is estimated to be 90 m (295 ft) per hour via automatic navigation, however, average traverse speeds will likely be about 30 m/h (98 ft/h), based on variables including power levels, difficulty of the terrain, slippage, and visibility. The metre or meter is a unit of Length. It is the basic unit of Length in the Metric system and in the International MSL is expected to traverse a minimum of 6 km (3. 7 mi) in its two-year mission.
At present 10 instruments have been selected for development or production for MSL:
All cameras are being developed by Malin Space Science Systems; all share common design components such as on-board electronic imaging processing boxes and 1600x1200 color CCDs. Malin Space Science Systems (or MSSS) is a San Diego, California company that designs develops and operates instruments to fly on unmanned spacecraft A charge-coupled device ( CCD) is an analog Shift register, that enables the transportation of analog signals (electric charges through successive stages (capacitors
ChemCam is a remote Laser-induced breakdown spectroscopy (LIBS) system that can target a rock from up to 13 meters away, vaporizing a small amount of the underlying mineral and then collecting a spectrum of the light emitted by the vaporized rock by using a micro-imaging camera with an angular resolution of 80 microradians. Laser-induced breakdown spectroscopy (LIBS is a type of atomic emission Spectroscopy which utilises a highly energetic Laser pulse as the excitation source The radian is a unit of plane Angle, equal to 180/ π degrees, or about 57 It is being developed by the Los Alamos National Laboratory and the French CESR laboratory (in charge of the laser). Los Alamos National Laboratory (LANL (previously known at various times as Site Y, Los Alamos Laboratory, and Los Alamos Scientific Laboratory) is a A infrared laser with 1067 nm wavelength and a 5 ns pulse will focus on a spot with 1 GW/cm², depositing 30 mJ of energy. Detection will be done between 240 nm and 800 nm. [5] [6] [7] In October 2007 NASA announced that they would cap funding for the ChemCam because of a 70% cost overrun and that the instrument has to be built with the money already provided. [8] Since most of the money for ChemCam came from the French CNES, The Los Alamos National Laboratory was able to deliver the engineering model to JPL in February 2008. [9]
This device will irradiate samples with alpha particles and map the spectra of X-rays that are reemitted. APXS is also an abbreviation for AP ache e' X' ten' S' ion tool an extension for Apache web servers Alpha particles (named after and denoted by the first letter in the Greek alphabet, α consist of two Protons and two Neutrons bound together into a X-radiation (composed of X-rays) is a form of Electromagnetic radiation. It is being developed by the Canadian Space Agency for determining the elemental composition of samples. The Canadian Space Agency ( CSA or in French, l' Agence spatiale canadienne, ASC) is the Canadian government The APXS is a form of PIXE. Particle-Induced X-ray Emission or Proton Induced X-ray Emission ( PIXE) is a technique used in the determining of the elemental make-up of a material or Similar instruments have been part of Mars Pathfinder and the Mars Exploration Rovers. The Mars Pathfinder was launched on December 4, 1996 by NASA aboard a Delta II just a month after the Mars Global Surveyor NASA 's Mars Exploration Rover ( MER) Mission is an ongoing robotic mission of exploring Mars, that began in 2003 with the sending of [10]
Chemin stands for "Chemistry & Mineralogy X-Ray Diffraction/X-Ray Fluorescence Instrument". Chemin is a X-ray diffraction/X-ray fluorescence instrument that will quantify minerals and mineral structure of samples. X-ray scattering techniques are a family of non-destructive analytical techniques which reveal information about the crystallographic structure chemical composition X-ray fluorescence (XRF is the emission of characteristic "secondary" (or fluorescent X-rays from a material that has been excited by bombarding with high-energy It is being developed by Dr. David Blake at NASA Ames Research Center and the NASA Jet Propulsion Laboratory. NASA Ames Research Center (ARC is a NASA facility located at Moffett Federal Airfield, which covers 43 acres at the borders of the cities of Mountain View [11]
The SAM instrument suite will analyze organics and gases from both atmospheric and solid samples. It is being developed by the NASA Goddard Space Flight Center and Laboratoire Inter-Universitaire des Systèmes Atmosphériques (LISA). The Goddard Space Flight Center ( GSFC) is a major NASA space research laboratory established on May 1, 1959 as NASA's first space flight [12]
SAM Consists of the 74 sample cups of the Sample Manipulation System[13] which can be heated to a temperature of 1000°C and the Chemical Separation and Processing Lab for enrichment and derivatization of the organic molecules of the sample. The gas chromatograph mass spectrometer is a quadrupole mass spectrometer with a mass range of 2–235 u which gets the sample from one of the six gas chromatography columns. Gas chromatography-mass spectrometry ( GC-MS) is a method that combines the features of Gas-liquid chromatography and Mass spectrometry to identify different The unified atomic mass unit ( u) or Dalton ( Da) or sometimes universal mass unit, is an unit of Mass used to express The Tunable Laser Spectrometer is capable of measuring the isotope ratios of carbon and oxygen in CO2.
This instrument will characterize the broad spectrum of radiation found near the surface of Mars for purposes of determining the viability and shielding needs for human explorers. Funded by the Exploration Systems Mission Directorate at NASA Headquarters and developed by Southwest Research Institute (SwRI) and the extraterrestrial physics group at Christian-Albrechts-Universität zu Kiel, Germany.
A pulsed neutron source and detector for measuring hydrogen or ice and water at or near the martian surface, provided by the Russian Federal Space Agency. The Russian Federal Space Agency ( Russian: Федеральное космическое агентство России Federal'noe kosmicheskoe agentstvo Rossii
Meteorological package and an ultraviolet sensor provided by the Spanish Ministry of Education and Science. Chief of State King Juan Carlos I, since November 22 1975; Queen Sofia Prince of Asturias Felipe It will be mounted on the camera mast and measure atmospheric pressure, humidity, wind currents and direction, air and ground temperature and ultraviolet radiation levels.
The MEDLI project’s main objective is to measure aerothermal environments, sub-surface heat shield material response, vehicle orientation, and atmospheric density for the atmospheric entry through the sensible atmosphere down to heatshield separation of the Mars Science Laboratory (MSL) entry vehicle. The MEDLI instrumentation suite will be installed in the heatshield of the MSL entry vehicle. The acquired data will support future Mars missions by providing measured atmospheric data to validate Mars atmosphere models and clarify the design margins on future Mars missions. MEDLI instrumentation consists of three main subsystems: MEDLI Integrated Sensor Plugs (MISP), Mars Entry Atmospheric Data System (MEADS), and the Sensor Support Electronics (SSE).
The rover will have the same type of engineering cameras that the MER rovers had, a stereo pair of Navcams used to select safe routes for driving and a set of front and rear stereo-pair Hazcams used for autonomous hazard avoidance during rover drives and for safe positioning of the robotic arm on rocks and soils. Hazcam is also the trade name of a self contained camera transmitter and battery pack designed for use around Hazardous materials and produced by Pragmatic
The rover will be powered by radioisotope thermoelectric generators (RTGs). NASA 's Mars Exploration Rover ( MER) Mission is an ongoing robotic mission of exploring Mars, that began in 2003 with the sending of A radioisotope thermoelectric generator ( RTG, RITEG) is an Electrical generator which obtains its power from Radioactive decay. Solar power is not an efficient power source for Mars surface operations. Solar energy is the Light and radiant heat from the Sun that powers Earth 's Climate and Weather and sustains Life Solar power systems cannot operate effectively at high Martian latitudes, in shaded areas, nor in dusty conditions. This limitation was emphasized by the July 2007 dust storms that nearly resulted in the permanent failure of the Mars Exploration Rovers. NASA 's Mars Exploration Rover ( MER) Mission is an ongoing robotic mission of exploring Mars, that began in 2003 with the sending of Furthermore, solar power cannot provide power at night, thus limiting the ability of the rover to keep its systems warm, reducing the life expectancy of electronics. Life expectancy is the average number of years of life remaining at a given age RTGs can provide reliable, continuous power day and night, and waste heat can be used via pipes to warm systems, freeing electrical power for the operation of the vehicle and instruments.
The first successful Mars landers, Viking 1 and Viking 2 in 1976, were RTG-powered—the Viking 1 lander worked for six years on the Martian surface (ultimately failing due to faulty command sent by ground control that resulted in loss of contact). Viking 1 was the first of two spacecraft sent to Mars as part of NASA 's Viking program, and holds the record for the longest Mars surface mission The Viking 2 mission was part of the Viking program to Mars, and consisted of an orbiter and a lander essentially identical to that of the Viking 1 The proposed power plant will use "next generation" RTGs, either Boeing’s Multi-mission Radioisotope Thermoelectric Generator, which is a more flexible and compact power system under development and based on conventional RTGs, or Lockheed Martin’s Stirling Radioisotope Generator, which is more efficient but untested for use in space. The Boeing Company is a major Aerospace and defense corporation originally founded by William E Lockheed Martin ( is a large multinational Aerospace manufacturer and advanced technology Company formed in 1995 by the merger of The Stirling radioisotope generator (SRG is based on a Stirling engine powered by a large Radioisotope heater unit. Evidence points to the MMRTG being selected at this point, likely because of reliability and underdevelopment issues with the SRG.
MSL will be set down on the Martian surface using a new NASA high-precision entry, descent, and landing (EDL) system that will place it within ten kilometers of an intended target, in contrast to the 150-kilometer error of previous landing systems used on Mars. The kilometre ( American spelling: kilometer) symbol km is a unit of Length in the Metric system, equal to one thousand The rover is folded up within an aeroshell which protects it during the travel through space and during the atmospheric entry at Mars. An aeroshell is a rigid Heat shielded shell that protects an entry vehicle during Spaceflight and from Atmospheric drag during landing Much of the reduction of the landing precision error is accomplished by an entry guidance algorithm, similar to that used by the astronauts returning to Earth in the Apollo space program. This guidance uses the lifting force experienced by the aeroshell to "fly out" any detected error in range and thereby arrive at the targeted landing site. In order for the aeroshell to have lift, its center of mass is offset from the axial centerline which results in an off-center trim angle in atmospheric flight, again similar to the Apollo Command Module. This is accomplished by a series of ejectable ballast mass. The lift vector is controlled by four sets of two Reaction Control System (RCS) thrusters that produce approximately 500 N of thrust per pair. A reaction control system, abbreviated RCS, is a subsystem of a Spacecraft. The newton (symbol N) is the SI derived unit of Force, named after Isaac Newton in recognition of his work on Classical This ability to change the pointing of the direction of lift allows the spacecraft to react to the ambient environment, and steer toward the landing zone.
After the entry phase is complete and the capsule has slowed to Mach 2 several kilometers over the ground, a supersonic parachute is deployed. Mach number (\mathrm{Ma} or M (generally ˈmɑːk sometimes /ˈmɑːx/ or /ˈmæk/ is the speed of an object moving through air or any Fluid A parachute is a device used to slow the motion of an object through an atmosphere by creating drag. The parachute is similar in design to that used by the Viking landers, Mars Pathfinder, and the Mars Exploration Rovers. The entry vehicle must first eject the ballast mass such that the center of gravity offset is removed and the velocity vector aligns with the parachute deployment vector. This prevents the spacecraft from experiencing a torque due to the pointing differences and increases the spacecraft's stability. A torque (τ in Physics, also called a moment (of force is a pseudo- vector that measures the tendency of a force to rotate an object about
Following the parachute deployment, the rover and descent stage drop out of the aeroshell. A number of passive mechanisms are used to ensure a clean separation. The descent stage is a platform above the rover with variable thrust mono propellant hydrazine rocket thrusters (based on upgraded Viking heritage landing rockets) on arms extending around this platform to slow the descent. Hydrazine is a Chemical compound with the formula N2H4 It has an Ammonia -like odor and is derived from the same industrial chemistry NASA 's Viking program consisted of a pair of space probes sent to Mars, Viking 1 and Viking 2. Meanwhile the rover itself is being transformed from its stowed flight configuration to a landing configuration while being lowered beneath the descent stage by the "sky crane" system. The descent stage contains the Bridle Umbilical Descent Rate Limiter (BUDrl) which is a next generation design based on MER heritage. NASA 's Mars Exploration Rover ( MER) Mission is an ongoing robotic mission of exploring Mars, that began in 2003 with the sending of This consists of 3 bridles lowering the rover itself and an umbilical cable carrying electrical signals between the descent stage and rover. At roughly 7. 5 meters below the descent stage the sky crane system slows to a halt and the rover touches down.
After the rover touches down it waits 2 seconds to confirm that it is on solid ground and fires several pyros (small explosive devices) activating cable cutters on the bridle and umbilical cords to free itself from the descent stage. The term "pyrotechnics" can also be used for Fireworks events The descent stage promptly flies away to a crash landing, and the rover gets ready to roam Mars.
Early landing system proposals for the rover featured a "pallet" design (similar to that used for Mars Pathfinder and the Mars Exploration Rovers) with a liquid-fueled rocket thruster system to land the rover in the final seconds of descent. A rocket or rocket vehicle is a Missile, Aircraft or other Vehicle which obtains Thrust by the reaction of the The pallet would have used airbags or a "crushable" design to permit a safe landing. An airbag is part of a vehicle's safety restraint system a flexible envelope designed for rapid inflation in an automobile Collision, to prevent vehicle occupants Earlier designs also sometimes included a second parachute for subsonic speeds. The planned "skycrane" powered descent landing system (as it has been referred) has never been used in actual missions before.
At the first MSL Landing Site workshop, 33 potential landing sites were identified. [14] The current engineering constraints call for a landing site less than 45° from the Martian equator and less than 1 km above the reference datum. This article describes a concept from Surveying and Geodesy. For other meanings see Datum (disambiguation. [15]
| Name | Location | Elevation | Target |
|---|---|---|---|
| Nili Fossae Trough | ≈22°N, ≈75°E | −0. Nili Fossae is a fracture in the surface of Mars that has been eroded and partly filled in by sediments and Clay -rich Ejecta from a nearby crater 6 km | Phyllosilicates |
| Holden Crater Fan | 26. The silicate minerals make up the largest and most important class of rock-forming Minerals They are classified based on the structure of their silicate Ion group Holden is a 140km wide crater on Mars, located with the southern highlands 4°S, 325. 3°E | −2. 3 km | Layered Materials |
| Terby Crater | 28°S, 73°E | −5 km | Layered Material |
| Mawrth Vallis | 22. In Geology and related fields a stratum (plural strata) is a layer of rock or Soil with internally consistent characteristics that distinguishes Terby is a crater on the northern edge of Hellas Planitia, Mars. Mawrth Vallis is a Valley on Mars at 223°N 3435°E with an elevation of ≈−2 km 3°N, 343. 5°E | ≈−2 km | Phyllosilicates |
| Eberswalde Crater | 24. Eberswalde crater, formerly known as Holden NE crater, is a partially buried Impact crater in Margaritifer Terra, Mars. 0°S, 326. 3°E | −0. 8 and −0. 4 km | Delta |
| Gale Crater | 4. A delta is a Landform where the mouth of a River flows into an Ocean, Sea, Estuary, Lake or another river Gale is a crater on Mars. It is about 150 km in diameter and is near the border of the lowlands of Elysium Planitia at. 6°S, 137. 2°E | −4. 5 km | Interior Layered Deposits |
| Candor Chasma | Various | −4 km | Sulfate Deposits |
| North Meridiani Planum | 2. Candor Chasma is one of the largest Canyons in the Valles Marineris canyon system on Mars. Meridiani Planum is a plain located 2 degrees south of Mars ' equator (centered at) in the westernmost portion of Terra Meridiani. 7°N, 358. 8°E | −1. 5 km | Sedimentary Layers |
| Juventae Chasma | 5°S, 297°E | −2 km | Layered Sulfates |
| Nilo Syrtis | ≈23°N, ≈76°E | ≈−0. Juventae Chasma is an enormous Box canyon (250 km × 100 km on Mars which opens to the north and forms the outflow channel Maja Vallis. Nilo Syrtis (or Nilosyrtis) is a region just north of Syrtis Major on Mars, at approximately 23°N 76°E and an elevation of −0 5 km | Phyllosilicates |
| Melas Chasma | 9. Melas Chasma is a Canyon on Mars, the widest segment of the Valles Marineris canyon system located east of Ius Chasma at 9 8°S, 283. 6°E | −1. 9 km | Paleolake |
| East Meridiani Planum | 0°, 3. 7°E | ≈−1. 3 km | Sedimentary Layers |
| Athabasca Vallis | 10°N, ?°E | −2. Athabasca Valles is a Valley on Mars, the youngest known channel cut into its surface by catastrophic Flooding The flood produced distinctive "teardrop" 4 km | Cerberus Rupes Deposits |
| Iani Chaos | 2°S , ≈342°E | Below −2 km | Hematite, Sulfate |
| Crater in Nili Fossae | 18. Iani Chaos, the source region of Ares Vallis on Mars, is centered at ~342°E 2°S 4°N, 77. 68°E | −2. 6 km | Valley Networks, layers |
| Eos Chasma | ≈11°N, ≈320°E | ≈−4 km | Chert |
| Crater lake in Meridiani Planum | 5. Eos Chasma is a Chasma in the southern part of the Valles Marineris canyon system of Mars. 6°N, 358°E | ≈−1. 5 km | Crater lake sediments |
| NE Syrtis Major | ≈10°N, ≈70°E | ≈1 km | Volcanics |
| Basin in Margaritifer Terra | 12. Syrtis Major Planum is a "dark spot" (an Albedo feature) located in the boundary between the northern lowlands and southern highlands of Mars. Margaritifer Terra is an ancient heavily cratered region of Mars. 77°S, 338. 1°E | −2. 12 km | Fluvial Deposits |
| Eastern Melas Chasma | 11. 62°S, 290. 45°E | Below −2 km | Interior Layered Deposits |
| Hellas Planitia/Dao Vallis | 40°S, 85°E | Below −2 km | A major valley |
| Xanthe Terra/Hypanis Vallis | 11°N, 314°E | Below −2 km | Delta |
| Becquerel Crater | 21. False color of Hellas Planitiajpeg|thumb|220px|This elevation map shows the surrounding elevated debris ring]] Hellas Planitia, also known as the Hellas Impact Basin Dao Vallis is a valley on Mars that appears to have been carved by water Xanthe Terra is a large area on Mars, centered just north of the Martian equator Hypanis Vallis is a 270km Valley in Xanthe Terra on Mars at 11ºN 314ºE 8°N, 351°E | −2. 6 to −3. 8 km | Layered Sedimentary Rocks |
| SW Arabia Terra | 2–12°N, 355–348°E | −1 km | Sed. Arabia Terra is a large upland region in the north of Mars. It is densely cratered and heavily eroded Rocks, Methane |
| Gullies/Hale Crater | 35. 7°S, 323. 4°E | −2. 4 km | Gullies |
| W. Arabia Terra | 8. 9°N, 358. 8°E | −1. 2 km | Sedimentary Rocks |
| Argyre Planitia | 56. Argyre Planitia is a plain located in the Argyre Impact basin in the southern highlands of Mars. 8°S, 317. 7°E | −1. 5 km | Glacial Features |
| NW Slope Valleys | ≈0, 145°E | ≈−2 km | Flood Features |
| Western Meridiani Planum | 1. 8°S, 7. 6°E | ≈−1. 0 to −1. 5 km | Sediments, Hematite |
| Elysium Planitia/Avernus Colles | 1. Elysium Planitia is the second largest volcanic region on Mars, after Tharsis Montes. Avernus Colles is a region of fractured terrain on Mars on the southeast margin of Elysium Planitia, at 1 0°S, 169. 5°E | Below −2 km | High iron abundance |
| Meridiani Bench | 7. 5°N, 354°E | ≈−1 to −1. 5 km | Layered Sediments |
| SML Craters | 49°S, 14°E | Above −0. 5 km | Recent Climate Deposits |
| Isidis Planitia Escarpment | 5–15°N, 80–95°E | Below −2 km | Volatile sink |
In late 2007, the list was reduced to six,[16] one of which (Miyamoto crater, on the southwest corner of Meridiani Planum) was not on the first workshop list. Isidis Planitia is a plain located inside a giant impact basin on Mars, centered at. Also, the locations of some of the targets have been refined relative to the first list.
| Name | Location |
|---|---|
| Miyamoto Crater | 2. 9°S, 7°W |
| Nili Fossae Trough | 21°N, 74°E |
| Holden Crater Fan | 26. Nili Fossae is a fracture in the surface of Mars that has been eroded and partly filled in by sediments and Clay -rich Ejecta from a nearby crater Holden is a 140km wide crater on Mars, located with the southern highlands 4°S, 325. 3°E |
| North Meridiani Planum | 2°N, 357°E |
| Mawrth Vallis | 24°N, 341°E |
| Eberswalde Crater Delta | 24°S, 327°E |
M. K. Lockwood (2006). "Introduction: Mars Science Laboratory: The Next Generation of Mars Landers And The Following 13 articles ". Journal of Spacecraft and Rockets 43: 257-257.