Developing Complex Systems to Advance Space Exploration:
- J. Douglas McCuistion
Director, Mars Exploration Program NASA Headquarters
http://www.nasa.gov/mars
July 10, 2012 Farnborough International Airshow
NASA’s Mars Exploration Program
Advance Space Exploration : Mars Science Laboratory/Curiosity J. - - PowerPoint PPT Presentation
NASAs Mars Exploration Program Developing Complex Systems to Advance Space Exploration : Mars Science Laboratory/Curiosity J. Douglas McCuistion Director, Mars Exploration Program NASA Headquarters http://www.nasa.gov/mars July 10, 2012
Director, Mars Exploration Program NASA Headquarters
http://www.nasa.gov/mars
July 10, 2012 Farnborough International Airshow
NASA’s Mars Exploration Program
MRO Mars Express Collaboration Odyssey Spirit & Opportunity
2009 2007
Phoenix (completed) MSL/Curiosity MAVEN
2005 2011 2013 2016 & Beyond
Mars future planning underway!
2003 2001
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OMEGA (300-1000 m/pixel) discovers first large phyllosilicate deposits CRISM targeted hyperspectral (20 m/pixel) characterizes deposits
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MGS Resolution (approx. 1.4 m/pixel)
Surtsey Island, Iceland
MRO Resolution (approx. 30 cm/pixel)
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Sojourner Spirit & Opportunity Curiosity Rover Mass 10.5 kg 174 kg 950 kg Driving Distance (req’t/actual) 10m/102m 600m / 31,468m 20,000m/TBD Mission Duration (req’t/actual) 10 sols/ 83 sols 90 sols/ 2,663 sols 687 sols/TBD Power / Sol 130 w/hr 499-950 w/hr ~2500 w/hr Instruments / Mass 1 / <1.5 kg 7 / 5.5 kg 10 / 75 kg Data Return 2.9 Mb/sol 50-150 Mb/sol 100-400 Mb/sol EDL Ballistic Entry Ballistic Entry Guided Entry
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Rover Flight Chassis & Harnessing
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SAM Flight Instrument
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The data/information contained herein has been reviewed and approved for release by JPL Export Administration on the basis that this document contains no export-controlled information.
Cruise Stage Backshell Descent Stage Rover Heatshield
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Approximate landing ellipse capability for the Opportunity and Spirit rovers Landing ellipse for the Curiosity Rover
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Fan
Layered Hard Rock
Clays
Younger Strata Fresh Craters Cemented Fractures
Milliken et al., 2010 Anderson and Bell, 2010
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DAN REMS ChemCam Mastcam RAD MAHLI APXS Brush Drill / Sieves Scoop MARDI
ROVER INSTRUMENTS
atmospheric opacity
composition; remote micro-imaging
composition, including organics
ENTRY, DESCENT and LANDING SYSTEM
ROVER INFRASTRUCTURE
s/w solutions
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= International partnership = International provision = US development
SAM Heat shield Backshell High Gain Antenna
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Information included herein may contain controlled information under the U.S. Government Export Laws. U.S. recipient is responsible for ensuring that no unauthorized export of controlled information takes place.
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26 Days to Landing August 5, 2012 PDT http://www.nasa.gov/mars