Mars Science Laboratory

Mars Science Laboratory
MSL concept February 2007 - PIA09201.jpg
2007 Mars Science Laboratory concept
Operator NASA
Major contractors Boeing, Lockheed Martin
Mission type Rover
Orbital insertion date lands between August 6 and August 20, 2012[1]
Launch date between November 25 and December 18, 2011[1]
Launch vehicle Atlas V 541
Mission duration 668 Martian sols (686 Earth days)
Homepage Mars Science Laboratory
Mass 1,984 pounds (900 kg)
Power RTG
Schematic diagram of the planned rover components.

The Mars Science Laboratory (MSL), known as Curiosity,[2][3] is a NASA rover scheduled to be launched in November 2011[4] and would perform the first-ever precision landing on Mars in August 2012. It is a rover that will assess whether Mars ever was, or is still today, an environment able to support microbial life. In other words, its mission is to determine the planet's habitability. It will also analyze samples scooped up from the soil and drilled powders from rocks.[5]

The MSL rover will be over five times as heavy as and carry over ten times the weight of scientific instruments as the Spirit or Opportunity rovers.[6] The United States, Canada, Germany, France, Russia and Spain will provide the instruments on board. The MSL rover will be launched by an Atlas V 541 rocket and will be expected to operate for at least 1 Martian year (668 Martian sols/686 Earth days) as it explores with greater range than any previous Mars rover.

Mars Science Laboratory is part of NASA's Mars Exploration Program, a long-term effort of robotic exploration of Mars, and is a project managed by NASA's Jet Propulsion Laboratory. The total cost of the MSL project is about $2.3 billion USD.[7]

Contents

Goals and objectives

The MSL has four goals: To determine if life ever arose on Mars, to characterize the climate of Mars, to characterize the geology of Mars, and to prepare for human exploration. To contribute to the four science goals and meet its specific goal of determining Mars' habitability, Mars Science Laboratory has eight scientific objectives:[8][9]

  1. Determine the nature and inventory of organic carbon compounds.
  2. Inventory the chemical building blocks of life as we know it: carbon, hydrogen, nitrogen, oxygen, phosphorus and sulfur.
  3. Identify features that may represent the effects of biological processes.
  4. Investigate the chemical, isotopic, and mineralogical composition of the Martian surface and near-surface geological materials.
  5. Interpret the processes that have formed and modified rocks and soils.
  6. Assess long-timescale (i.e., 4-billion-year) Martian atmospheric evolution processes.
  7. Determine present state, distribution, and cycling of water and carbon dioxide.
  8. Characterize the broad spectrum of surface radiation, including galactic radiation, cosmic radiation, solar proton events and secondary neutrons.

History

Jet Propulsion Laboratory engineers test and assemble Curiosity in a large clean room on June 29, 2010 in preparation for a late 2011 launch

In April 2008, it was reported that the project was $235 million USD, or 24% over budget and that the money to compensate this overrun may have to come from other NASA Mars missions.[6]

In October 2008, MSL was getting closer to a 30% cost overrun.[10][11]

On November 19, 2008, NASA announced that MSL project leaders at the Jet Propulsion Laboratory (JPL) had reduced the list of candidate landing sites to four: Eberswalde, Gale, Holden, Mawrth.[12]

As of November 2008, development is essentially finished, much of MSL hardware and software are complete and testing is ongoing.[13]

On December 3, 2008, NASA announced that the MSL launch will be delayed until the fall of 2011 because of inadequate test time.[14] The technical and budgetary reasons behind the delay were explained to the Planetary Science Community in a January 2009 meeting at NASA Headquarters.[15][16]

From March 23–29, 2009, the general public had an opportunity to rank nine finalist names through a public poll on the NASA website as additional input for judges to consider during the MSL name selection process.[2] On May 27, 2009, the winning name of Curiosity, which was submitted by a sixth-grader, Clara Ma, from Kansas was chosen.[2][3][17]

In late June 2010, engineers completed the installation of the suspension and wheel assembles on the rover body. The six-wheeled rocker-bogie suspension is similar to design found on Mars Exploration Rovers and Mars Pathfinder rover. Engineers began testing the integrated suspension system which will also serve as landing gear for the vehicle unlike its smaller predecessors.[18]

Specifications

MSL mockup compared with the Mars Exploration Rover and Sojourner rover by the Jet Propulsion Laboratory on May 12, 2008
A comparison of sizes for the Sojourner rover, the Mars Exploration Rovers, the Phoenix Lander and the Mars Science Laboratory.
The MSL Assembly, Test and Launch Operations (ATLO) in the Jet Propulsion Laboratory
Wheel size comparison: Sojourner, Mars Exploration Rover, Mars Science Laboratory

Length/weight

The MSL will have a length of 9 feet (2.7 m) and weigh 1,984 pounds (900 kg) including 176 pounds (80 kg) of scientific instruments.[6] It will be the same size as a Mini Cooper automobile.[19] This compares to the Mars Exploration Rovers which have a length of 5 feet 2 inches (1.57 m) and weigh 384 pounds (174 kg) including 15 pounds (6.8 kg) of scientific instruments.[6][20]

Speed

Once on the surface, the MSL rover will be able to roll over obstacles approaching 75 centimeters (30 in) high. Maximum terrain-traverse speed is estimated to be 90 meters (300 ft) per hour via automatic navigation, however, average traverse speeds will likely be about 30 meters (100 ft) per hour, based on variables including power levels, difficulty of the terrain, slippage, and visibility. MSL is expected to traverse a minimum of 12 miles (19 km) in its two-year mission.[21]

Power source

The MSL will be powered by radioisotope thermoelectric generators (RTGs), as used by the successful Mars landers Viking 1 and Viking 2 in 1976.[22][23] Radioisotope power systems are generators that produce electricity from the natural decay of plutonium-238, which is a non-weapons-grade form of that radioisotope used in power systems for NASA spacecraft. Heat given off by the natural decay of this isotope is converted into electricity, providing constant power during all seasons and through the 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.[22][23]

The MSL power source will use the latest RTG generation built by Boeing, called the "Multi-Mission Radioisotope Thermoelectric Generator" (MMRTG).[24] The MMRTG is a flexible and compact power system under development that is based on conventional RTGs.[24] The MMRTG is designed to produce 125 watts of electrical power at the start of the mission and 100 watts after 14 years.[25] The MSL will generate 2.5 kilowatt hours per day compared to the Mars Exploration Rovers which can generate about 0.6 kilowatt hours per day.[6] Although the primary mission is planned to last about 2 Earth years, the MMRTG will have a minimum lifetime of 14 years.[26]

Heat Rejection System

The temperatures in the potential areas at which the MSL may land can vary from +86°F to −197°F (+30 to −127°C). Therefore, the Heat Rejection System (HRS) uses fluid pumped through 60m (200 feet) of tubes in the MSL body so that sensitive components are kept at optimal temperatures.[27] Other methods of heating the internal components include using radiated heat generated from the components in the craft itself, as well as excess heat from the MMRTG unit. The HRS also has the ability to cool components if necessary.[28]

Computers

The two identical on-board rover computers, called "Rover Electronics Module" (REM), contain radiation hardened memory to tolerate the extreme radiation environment from space and to safeguard against power-off cycles. Each computer's memory includes 256 kB of EEPROM, 256 MB of DRAM, and 2 GB of flash memory.[29] This compares to 3 MB of EEPROM, 128 MB of DRAM, and 256 MB of flash memory used in the Mars Exploration Rovers.[30]

The REM computers use the RAD750 CPU which is a successor to the RAD6000 CPU used in the Mars Exploration Rovers.[31][32] The RAD750 CPU is capable of up to 400 MIPS while the RAD6000 CPU is capable of up to 35 MIPS.[33][34]

The rover has an Inertial Measurement Unit (IMU) that provides 3-axis information on its position which is used in rover navigation.[29] The rover's computers are constantly self-monitoring to keep the rover operational, such as by regulating the rover's temperature.[29] Activities such as taking pictures, driving, and operating the instruments are performed in a command sequence that is sent from the flight team to the rover.[29] In the event of problems with the main computer, the backup computer will take over.[29]

Proposed payload

At present, 10 instruments have been selected for development or production for the Mars Science Laboratory rover:

Cameras (MastCam, MAHLI, MARDI)

The MastCam, MAHLI, and MARDI cameras are being developed by Malin Space Science Systems and they all share common design components, such as on-board electronic imaging processing boxes, 1600x1200 CCDs, and a RGB Bayer pattern filter.[35][36][37][38][39]

ChemCam

ChemCam is a suite of remote sensing instruments, including the first laser-induced breakdown spectroscopy (LIBS) system to be used for planetary science and a remote micro-imager (RMI).[41][42] The LIBS instrument can target a rock or soil sample from up to 7 meters away, vaporizing a small amount of it and then collecting a spectrum of the light emitted by the vaporized rock.[41] An infrared laser with 1067 nm wavelength and a 5 nanosecond pulse will focus on a sub-millimeter spot with a power in excess of 10 megawatts, depositing 15mJ of energy.[41] Detection of the ball of luminous plasma will be done in the visible and near-UV and near-IR range, between 240 nm and 800 nm.[41] Using the same collection optics, the RMI provides context images of the LIBS analysis spots.[41] The RMI resolves 1 mm objects at 10 m distance, and has a field of view covering 20 cm at that distance.[41] The ChemCam instrument suite is being developed by the Los Alamos National Laboratory and the French CESR laboratory.[41][43][44][45] NASA's cost for ChemCam is approximately $10M, including an overrun of about $1.5M,[46] which is about 4% of the total mission costs.[47] The flight model of the Mast Unit was delivered from the French CNES to Los Alamos National Laboratory and was able to deliver the engineering model to JPL in February 2008.[48]

Alpha-particle X-ray spectrometer (APXS)

This device will irradiate samples with alpha particles and map the spectra of X-rays that are reemitted for determining the elemental composition of samples.[49] It is being developed by the Canadian Space Agency.[49] The APXS is a form of PIXE, which has previously been used by the Mars Pathfinder and the Mars Exploration Rovers.[49][50]

CheMin

Chemin stands for "Chemistry and Mineralogy" and is a X-Ray diffraction/X-Ray fluorescence instrument[51] that will quantify minerals and mineral structure of samples.[51] It is being developed by Dr. David Blake at NASA Ames Research Center and the NASA's Jet Propulsion Laboratory.[51][52]

Sample Analysis at Mars (SAM)

The SAM instrument suite will analyze organics and gases from both atmospheric and solid samples.[53][54] It is being developed by the NASA Goddard Space Flight Center, the Laboratoire Inter-Universitaire des Systèmes Atmosphériques (LISA) of France's CNRS and Honeybee Robotics, along with many additional external partners.[53][55][56] The SAM suite consists of three instruments:

The Quadrupole Mass Spectrometer (QMS) will detect gases sampled from the atmosphere or those released from solid samples by heating.[53] The Gas Chromatograph (GC) will be used to separate out individual gases from a complex mixture into molecular components with a mass range of 2–235 u.[53] The Tunable Laser Spectrometer (TLS) will perform precision measurements of oxygen and carbon isotope ratios in carbon dioxide (CO2) and methane (CH4) in the atmosphere of Mars in order to distinguish between a geochemical and a biological origin.[53][56][57][58]

The SAM also has three subsystems: The Chemical Separation and Processing Laboratory (CSPL), for enrichment and derivatization of the organic molecules of the sample; the Sample Manipulation System (SMS) for transporting powder delivered from the MSL drill to a SAM inlet and into one of 74 sample cups.[53] The SMS then moves the sample to the SAM oven to release gases by heating to up to 1000 oC;[53][59] and the Wide Range Pumps (WRP) subsystem to purge the QMS, TLS, and the CPSL.

Radiation Assessment Detector (RAD)

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.[60] Funded by the Exploration Systems Mission Directorate at NASA Headquarters and the German space agency, DLR, RAD was developed by Southwest Research Institute (SwRI) and the extraterrestrial physics group at Christian-Albrechts-Universität zu Kiel, Germany.[60]

Dynamic Albedo of Neutrons (DAN)

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.[61]

Rover Environmental Monitoring Station (REMS)

Meteorological package and an ultraviolet sensor provided by the Spanish Ministry of Education and Science.[62] 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.[62]

MSL Entry Descent and Landing Instrumentation (MEDLI)

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 heat shield separation of the Mars Science Laboratory entry vehicle.[63][64] The MEDLI instrumentation suite will be installed in the heatshield of the MSL entry vehicle.[63][64] 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.[63][64] MEDLI instrumentation consists of three main subsystems: MEDLI Integrated Sensor Plugs (MISP), Mars Entry Atmospheric Data System (MEADS) and the Sensor Support Electronics (SSE).[63][64]

Hazard Avoidance Cameras (Hazcams)

The MSL will use two pairs of black and white navigation cameras located on the front left and right and rear left and right of the rover.[65][66] The Hazard Avoidance Cameras (also called Hazcams) are used for autonomous hazard avoidance during rover drives and for safe positioning of the robotic arm on rocks and soils.[65] The cameras will use visible light to capture stereoscopic three-dimensional (3-D) imagery.[65] The cameras have a 120 degree field of view and map the terrain at up to 10 feet (3 meters) in front of the rover.[65] This imagery safeguards against the rover inadvertently crashing into unexpected obstacles, and works in tandem with software that allows the rover to make its own safety choices.[65]

Navigation Cameras (Navcams)

The MSL will use a pair of black and white navigation cameras mounted on the mast to support ground navigation.[66][67] The cameras will use visible light to capture stereoscopic 3-D imagery.[67] The cameras have a 45 degree field of view.[67]

Launch vehicle

The MSL will be launched using the Atlas V 541 which is a two stage rocket capable of launching up to 17,597 pounds (8,672 kg) to geostationary transfer orbit. The Atlas V has also been used to launch the Mars Reconnaissance Orbiter and New Horizons.[68]

Landing system

MSL landing diagram for outside Martian atmosphere and for entry.
MSL landing diagram for parachute descent, powered descent, and sky crane.

Landing a large mass on Mars is a difficult challenge: the atmosphere is thick enough to prevent rockets being used to provide significant deceleration, but too thin for parachutes and aerobraking alone to be effective.[69] Although some previous missions have used airbags to cushion the shock of landing, the MSL is too large for this to be an option.

The MSL will be set down on the Martian surface using a new high-precision entry, descent, and landing (EDL) system that will place it in a 20 kilometer (12 mile) landing ellipse, in contrast to the 150 kilometer by 20 kilometer (about 93 miles by 12 miles) landing ellipse of the landing systems used by the Mars Exploration Rovers.[70]

For this, the MSL will employ a combination of several systems in a precise order, where the entry, descent and landing sequence will break down into four parts.[71][72]

The MSL test parachute. Note the people in the lower-right corner of the image.

Proposed landing sites

The essential issue when selecting an optimum landing site, is to identify a particular geologic environment, or set of environments, that would support microbial life. To mitigate the risk of disappointment and ensure the greatest chance for science success, interest is placed at the greatest number of possible science objectives at a chosen landing site. Thus, a landing site with morphologic and mineralogic evidence for past water, is better than a site with just one of these criteria. Furthermore, a site with spectra indicating multiple hydrated minerals is preferred; clay minerals and sulfate salts would constitute a rich site. Hematite, other iron oxides, sulfate minerals, silicate minerals, silica, and possibly chloride minerals have all been suggested as possible substrates for fossil preservation. Indeed, all are known to facilitate the preservation of fossil morphologies and molecules on Earth.[76] Difficult terrain is the best candidate for finding evidence of livable conditions, and engineers must be sure the rover can safely reach the site and drive within it.[77]

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.[78] At the first MSL Landing Site workshop, 33 potential landing sites were identified.[79] By the second workshop in late 2007, the list had grown to include almost 50 sites,[80] and by the end of the workshop, the list was reduced to six;[81] [82][83] in November 2008, project leaders at a third workshop reduced the list to four landing sites.[84]

On August 20, 2009, NASA sent out a call for additional landing site proposals. The new proposals will be evaluated and reviewed until the summer of 2010.[85] A fourth landing site workshop, taking both the new and existing proposals into account, is planned for September 2010. The fifth and final workshop is planned for March 2011.[86]

Current prospective landing sites[87][88]
Name Location
Eberswalde Crater Delta 24.0°S, 327.0°E
Holden Crater Fan 26.4°S, 325.3°E
Gale Crater   4.6°S, 137.2°E
Mawrth Vallis 24.0°N, 341.0°E

See also

References

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  2. ↑ 2.0 2.1 2.2 "Name NASA's Next Mars Rover". NASA/JPL. 2009-05-27. http://marsrovername.jpl.nasa.gov/. Retrieved 2009-05-27. 
  3. ↑ 3.0 3.1 "NASA Selects Student's Entry as New Mars Rover Name". NASA/JPL. 2009-05-27. http://www.nasa.gov/mission_pages/msl/msl-20090527.html. Retrieved 2009-05-27. 
  4. ↑ "NASA's Shuttle and Rocket Launch Schedule". NASA. 2010-10-27. http://www.nasa.gov/missions/highlights/schedule.html. Retrieved 2010-09-02. 
  5. ↑ "Mars Science Laboratory: Mission". NASA/JPL. http://marsprogram.jpl.nasa.gov/msl/mission/. Retrieved 2010-03-12. 
  6. ↑ 6.0 6.1 6.2 6.3 6.4 Watson, Traci (2008-04-14). "Troubles parallel ambitions in NASA Mars project". USA Today. http://www.usatoday.com/tech/science/space/2008-04-13-mars_N.htm. Retrieved 2009-05-27. 
  7. ↑ Chang, Kenneth (2008-12-04). "NASA Delays Next Mars Rover Mission". The New York Times. http://www.nytimes.com/2008/12/05/science/space/05mars.html. Retrieved 2009-05-27. 
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  9. ↑ Mars Science Laboratory Mission Profile
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  20. ↑ A YouTube video shows a MSL mockup compared to the Mars Exploration Rover and Sojourner Rover. "Mars Rovers". YouTube. 2008-04-12. http://www.youtube.com/watch?v=D7kBTZAGhbs. Retrieved 2008-09-12. 
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  23. ↑ 23.0 23.1 "Mars Exploration: Radioisotope Power and Heating for Mars Surface Exploration". NASA/JPL. 2006-04-18. http://www.jpl.nasa.gov/news/fact_sheets/mars-power-heating.pdf. Retrieved 2009-09-07. 
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  35. ↑ 35.0 35.1 35.2 35.3 35.4 35.5 35.6 "Mast Camera (Mastcam)". NASA/JPL. http://msl-scicorner.jpl.nasa.gov/Instruments/Mastcam/. Retrieved 2009-03-18. 
  36. ↑ 36.0 36.1 36.2 36.3 36.4 36.5 36.6 "Mars Hand Lens Imager (MAHLI)". NASA/JPL. http://msl-scicorner.jpl.nasa.gov/Instruments/MAHLI/. Retrieved 2009-03-23. 
  37. ↑ 37.0 37.1 37.2 37.3 37.4 "Mars Descent Imager (MARDI)". NASA/JPL. http://msl-scicorner.jpl.nasa.gov/Instruments/MARDI/. Retrieved 2009-04-03. 
  38. ↑ 38.0 38.1 38.2 "Mars Science Laboratory (MSL): Mast Camera (Mastcam): Instrument Description". Malin Space Science Systems. http://www.msss.com/msl/mastcam/MastCam_description.html. Retrieved 2009-04-19. 
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  44. ↑ CESR presentation on the LIBS
  45. ↑ ChemCam fact sheet
  46. ↑ Wiens R.C., Maurice S. (2008). "Corrections and Clarifications, News of the Week". Science 322 (5907): 1466. doi:10.1126/science.322.5907.1466a. PMID 19056960. http://www.sciencemag.org. 
  47. ↑ Wiens R.C., Maurice S. (2008). "ChemCam's Cost a Drop in the Mars Bucket". Science 322 (5907): 1464. doi:10.1126/science.322.5907.1464a. PMID 19056957. http://www.sciencemag.org. 
  48. ↑ ChemCam Status April, 2008
  49. ↑ 49.0 49.1 49.2 "MSL Science Corner: Alpha Particle X-ray Spectrometer (APXS)". NASA/JPL. http://msl-scicorner.jpl.nasa.gov/Instruments/APXS/. Retrieved 2009-09-09. 
  50. ↑ R. Rieder, R. Gellert, J. Brückner, G. Klingelhöfer, G. Dreibus, A. Yen, S. W. Squyres (2003). "The new Athena alpha particle X-ray spectrometer for the Mars Exploration Rovers". J. Geophysical Research 108: 8066. doi:10.1029/2003JE002150. 
  51. ↑ 51.0 51.1 51.2 "MSL Science Corner: Chemistry & Mineralogy (CheMin)". NASA/JPL. http://msl-scicorner.jpl.nasa.gov/Instruments/CheMin/. Retrieved 2009-09-09. 
  52. ↑ Sarrazin P., Blake D., Feldman S., Chipera S., Vaniman D., Bish D. (2005). "Field deployment of a portable X-ray diffraction/X-ray flourescence instrument on Mars analog terrain". Powder Diffraction 20 (2): 128–133. doi:10.1154/1.1913719. 
  53. ↑ 53.0 53.1 53.2 53.3 53.4 53.5 53.6 "MSL Science Corner: Sample Analysis at Mars (SAM)". NASA/JPL. http://msl-scicorner.jpl.nasa.gov/Instruments/SAM/. Retrieved 2009-09-09. 
  54. ↑ Overview of the SAM instrument suite
  55. ↑ Cabane M., Coll P., Szopa C., Israel G., Raulin F., Sternberg R., Mahaffy P., Person A., Rodier C., Navarro-Gonzalez R., Niemann H., Harpold D., Brinckerhoff W. (2004). "Did life exist on Mars? Search for organic and inorganic signatures, one of the goals for "SAM" (sample analysis at Mars)". Source: Mercury, Mars and Saturn Advances in Space Research 33 (12): 2240–2245. 
  56. ↑ 56.0 56.1 "Sample Analysis at Mars (SAM) Instrument Suite". NASA. October 2008. http://ael.gsfc.nasa.gov/marsSAM.shtml. Retrieved 2008-10-09. 
  57. ↑ Tenenbaum, David (June 09, 2008):). "Making Sense of Mars Methane". Astrobiology Magazine. http://www.astrobio.net/news/modules.php?op=modload&name=News&file=article&sid=2765&mode=thread&order=0&thold=0. Retrieved 2008-10-08. 
  58. ↑ Tarsitano, C.G. and Webster, C.R. (2007). "Multilaser Herriott cell for planetary tunable laser spectrometers". Applied Optics, 46 (28): 6923–6935. doi:10.1364/AO.46.006923. 
  59. ↑ Tom Kennedy and Erik Mumm, Tom Myrick , Seth Frader-Thompson. "Optimization of a mars sample manipulation system through concentrated functionality" (PDF). http://pdf.aiaa.org/preview/CDReadyMSPACE06_1393/PV2006_7402.pdf. 
  60. ↑ 60.0 60.1 "MSL Science Corner: Radiation Assessment Detector (RAD)". NASA/JPL. http://msl-scicorner.jpl.nasa.gov/Instruments/RAD/. Retrieved 2009-09-09. 
  61. ↑ "MSL Science Corner: Dynamic Albedo of Neutrons (DAN)". NASA/JPL. http://msl-scicorner.jpl.nasa.gov/Instruments/DAN/. Retrieved 2009-09-09. 
  62. ↑ 62.0 62.1 "MSL Science Corner: Rover Environmental Monitoring Station (REMS)". NASA/JPL. http://msl-scicorner.jpl.nasa.gov/Instruments/REMS/. Retrieved 2009-09-09. 
  63. ↑ 63.0 63.1 63.2 63.3 Michael Wright (2007-05-01). "Science Overview System Design Review (SDR)". NASA/JPL. http://www.mrc.uidaho.edu/~atkinson/SeniorDesign/ThermEx/MEDLI/MEDLI_SDR_Project_Overview.pdf. Retrieved 2009-09-09. 
  64. ↑ 64.0 64.1 64.2 64.3 Michael Wright (2007-05-01). "Science Overview System Design Review (SDR)". NASA/JPL. http://www.mrc.uidaho.edu/~atkinson/SeniorDesign/ThermEx/MEDLI/MEDLI_SDR_Science_Overview.pdf. Retrieved 2009-09-09. 
  65. ↑ 65.0 65.1 65.2 65.3 65.4 "Mars Science Laboratory: Mission: Rover: Eyes and Other Senses: Four Engineering Hazcams (Hazard Avoidance Cameras)". NASA/JPL. http://marsprogram.jpl.nasa.gov/msl/mission/rover/eyesandother/. Retrieved 2009-04-04. 
  66. ↑ 66.0 66.1 "Mars Science Laboratory Rover in the JPL Mars Yard". NASA/JPL. http://marsprogram.jpl.nasa.gov/msl/multimedia/interactives/photosynth/. Retrieved 2009-05-10. 
  67. ↑ 67.0 67.1 67.2 "Mars Science Laboratory: Mission: Rover: Eyes and Other Senses: Two Engineering Navcams (Navigation Cameras)". NASA/JPL. http://marsprogram.jpl.nasa.gov/msl/mission/rover/eyesandother/. Retrieved 2009-04-04. 
  68. ↑ "Mars Science Laboratory: Mission: Launch Vehicle". NASA/JPL. http://marsprogram.jpl.nasa.gov/msl/mission/launchvehicle/. Retrieved 2009-04-01. 
  69. ↑ "The Mars Landing Approach: Getting Large Payloads to the Surface of the Red Planet". Universe Today. http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/. Retrieved 2008-10-21. 
  70. ↑ 70.0 70.1 70.2 70.3 "Entry, Descent, and Landing". NASA/JPL. http://marsprogram.jpl.nasa.gov/msl/mission/timeline/edl/index.html. Retrieved 2009-09-07. 
  71. ↑ "Mission Timeline: Entry, Descent, and Landing". NASA and JPL. http://marsprogram.jpl.nasa.gov/msl/mission/tl_edl.html. Retrieved 2008-10-07. 
  72. ↑ "Mars Science Laboratory Entry, Descent, and Landing Triggers". IEEE. http://ieeexplore.ieee.org/stamp/stamp.jsp?arnumber=04161341. Retrieved 2008-10-21. 
  73. ↑ NASA, Large Heat Shield for Mars Science Laboratory, 07.10.09 (accessed Mar 26 2010)
  74. ↑ 74.0 74.1 74.2 "Mars Science Laboratory Parachute Qualification Testing". NASA/JPL. http://marsprogram.jpl.nasa.gov/msl/news/index.cfm?FuseAction=ShowNews&NewsID=90. Retrieved 2009-04-15. 
  75. ↑ Sky crane concept video
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  77. ↑ "Survivor: Mars — Seven Possible MSL Landing Sites". Jet Propulsion Laboratory (NASA). 18 September 2008. http://mars.jpl.nasa.gov/msl/spotlight/20080918.html. Retrieved 2008-10-21. 
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  89. ↑ "Final 7 Prospective Landing Sites". NASA. February 19, 2009. http://marsoweb.nas.nasa.gov/landingsites/index.html. Retrieved 2009-02-09. 

Further reading

M. K. Lockwood (2006). "Introduction: Mars Science Laboratory: The Next Generation of Mars Landers And The Following 13 articles " (PDF). Journal of Spacecraft and Rockets 43 (2): 257–257. doi:10.2514/1.20678. http://pdf.aiaa.org/jaPreview/JSR/2006/PVJA20678.pdf. 

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