Verification and Validation of the Mars Science Laboratory/Curiosity Rover Entry, Descent, and Landing System

On 6 August 2012, the Curiosity rover successfully touched down on the Martian surface setting off the most ambitious surface exploration of this planetary body. Preceding this significant step were years of design, development, and testing of the Curiosity Entry, Descent, and Landing system to prepare for the most complex landing endeavor ever attempted at Mars. To address the numerous challenges, the approach and implementation of the overall Entry, Descent, and Landing verification and validation program relied on its decomposition into three distinct domains: flight dynamics, flight system and subsystem verification and validation. The test and analysis scope, the venues, and the processes utilized were tailored to each of these domains, and are discussed in greater detail. The overall lessons learned and conclusions described herein can serve as a pathfinder for the Entry, Descent, and Landing system testing approach and implementation of future Mars landed missions.

[1]  W. J. Hurd,et al.  Critical spacecraft-to-Earth communications for Mars Exploration Rover (MER) entry, descent and landing , 2002, Proceedings, IEEE Aerospace Conference.

[2]  William I. Scallion,et al.  Aerodynamic Challenges for the Mars Science Laboratory Entry, Descent and Landing , 2009 .

[3]  Riley Duren Validation and verification of deep-space missions , 2004 .

[4]  Wayne Lee,et al.  Mars Exploration Rover Mission: Entry, Descent, and Landing System Validation , 2004 .

[5]  Karl T. Edquist,et al.  Aerothermodynamic Design of the Mars Science Laboratory Heatshield , 2009 .

[6]  Paul M. Siemers,et al.  Development of the Viking Parachute Configuration by Wind-Tunnel Investigation , 1973 .

[7]  Brian D. Pollard,et al.  A Radar Terminal Descent Sensor for the Mars Science Laboratory mission , 2009, 2009 IEEE Aerospace conference.

[8]  Gavin F. Mendeck,et al.  Entry Guidance for the 2011 Mars Science Laboratory Mission , 2011 .

[9]  Brian R. Hollis,et al.  Turbulent Aeroheating Testing of Mars Science Laboratory Entry Vehicle in Perfect-Gas Nitrogen , 2007 .

[10]  Matthew L. Rozek,et al.  Managing complexity in the MSL/Curiosity entry, descent, and landing flight software and avionics verification and validation campaign , 2013 .

[11]  Karl T. Edquist,et al.  Aerothermodynamic Design of the Mars Science Laboratory Backshell and Parachute Cone , 2009 .

[12]  Wayne Hathaway,et al.  Dynamic Stability Testing of the Mars Science Laboratory Entry Capsule , 2009 .

[13]  J. Gallon Verification and validation testing of the Bridle and Umbilical Device for Mars Science Laboratory , 2012, 2012 IEEE Aerospace Conference.

[14]  R. Mitcheltree,et al.  Mars Science Laboratory entry, descent and landing system verification and validation program , 2006, 2006 IEEE Aerospace Conference.

[15]  Karl T. Edquist,et al.  Development of the Mars Science Laboratory Heatshield Thermal Protection System , 2014 .

[16]  Kim P. Gostelow The Mars Science Laboratory Entry, Descent, and Landing Flight Software , 2013 .

[17]  F. M. Cheatwood,et al.  Mars Exploration Rover Six-Degree-Of-Freedom Entry Trajectory Analysis , 2006 .

[18]  Chia-Yen Peng,et al.  Analysis and Test Validation to Develop Mars Science Laboratory EDL Loads - Mobility Deploy Event , 2012 .

[19]  Jim Montgomery Implementing the Mars Science Laboratory Terminal Descent Sensor Field Test Campaign , 2012 .

[20]  A. Chen,et al.  Mars Science Laboratory Entry, Descent, and Landing System Overview , 2008, 2008 IEEE Aerospace Conference.

[21]  J. Balaram,et al.  Mars Science Laboratory Simulations for Entry, Descent, and Landing , 2006 .

[22]  David Henriquez,et al.  Workstation-Based Avionics Simulator to Support Mars Science Laboratory Flight Software Development , 2008 .

[23]  Matt Dawson,et al.  Monopropellant Hydrazine 700 lbf Throttling Terminal Descent Engine for Mars Science Laboratory , 2007 .

[24]  P. Daniel Burkhart,et al.  MSL DSENDS EDL Analysis and Operations , 2012 .

[25]  J.C. Gallon,et al.  Guide Rails for Linear Separation of Powered Descent Vehicle from Mars Science Laboratory Backshell , 2008, 2008 IEEE Aerospace Conference.

[26]  David M. Driver,et al.  Arc Jet Testing in a Shear Environment for Mars Science Laboratory Thermal Protection System , 2009 .

[27]  R. J. Bendura,et al.  Flight tests of Viking parachute system in three Mach number regimes. 2: Parachute test results , 1974 .

[28]  Pradeep Bhandari,et al.  Mars Science Laboratory Rover System Thermal Test , 2012 .

[29]  Jeffrey M. Weiss,et al.  Design and development of the MSL descent stage propulsion system , 2013 .

[30]  R. Mukai,et al.  Direct-to-Earth communications with Mars Science Laboratory during Entry, Descent, and Landing , 2013, 2013 IEEE Aerospace Conference.

[31]  Artem A. Dyakonov,et al.  Hypersonic and Supersonic Static Aerodynamics of Mars Science Laboratory Entry Vehicle , 2012 .

[32]  Douglas S. Adams,et al.  Mars Science Laboratory's Parachute Qualification Approach , 2009 .

[33]  Allen Witkowski,et al.  Findings from the supersonic qualification program of the Mars Science Laboratory parachute system , 2009 .

[34]  Gregory Carr,et al.  Mars Science Laboratory (MSL) Power System Architecture , 2012 .

[35]  D. Fort,et al.  Spacecraft-to-earth communications for Juno and Mars Science Laboratory critical events , 2012, 2012 IEEE Aerospace Conference.

[36]  Karl T. Edquist,et al.  Development of the Mars Science Laboratory Heatshield Thermal Protection System , 2009 .

[37]  David M. Driver,et al.  Arcjet Testing in Shear Environment for Mars Science Laboratory Thermal Protection System , 2014 .

[38]  A.M.S. Martin,et al.  Mars Science Laboratory: Entry, Descent, and Landing System Performance , 2007, 2007 IEEE Aerospace Conference.

[39]  C. A. Brown,et al.  Experimental wake survey behind Viking 75 entry vehicle at angles of attack of 0 deg, 5 deg, and 10 deg, Mach numbers from 0.20 to 1.20, and longitudinal stations from 1.50 to 11.00 body diameters , 1973 .

[40]  Sami W. Asmar,et al.  Reconstruction of Entry, Descent, and Landing Communications for the Phoenix Mars Lander , 2011 .

[41]  Jordan P. Evans Managing the Mars Science Laboratory Thermal Vacuum Test for safety and success , 2010, 2010 IEEE Aerospace Conference.

[42]  Chia-Yen Peng,et al.  System verification of MSL Skycrane using an integrated ADAMS simulation , 2012, 2012 IEEE Aerospace Conference.

[43]  William I. Scallion,et al.  Aerodynamic Interference Due to MSL Reaction Control System , 2009 .

[44]  David Hinson,et al.  Atmospheric risk assessment for the Mars Science Laboratory Entry, Descent, and Landing system , 2010, 2010 IEEE Aerospace Conference.

[45]  Jill L. Prince,et al.  Mars Phoenix Entry, Descent, and Landing Simulation Design and Modelling Analysis , 2011 .