Relay support for the Mars Science Laboratory mission

The Mars Science Laboratory (MSL) mission landed the Curiosity Rover on the surface of Mars on August 6, 2012, beginning a one-Martian-year primary science mission. An international network of Mars relay orbiters, including NASA's 2001 Mars Odyssey Orbiter (ODY) and Mars Reconnaissance Orbiter (MRO), and ESA's Mars Express Orbiter (MEX), were positioned to provide critical event coverage of MSL's Entry, Descent, and Landing (EDL). The EDL communication plan took advantage of unique and complementary capabilities of each orbiter to provide robust information capture during this critical event while also providing low-latency information during the landing. Once on the surface, ODY and MRO have provided effectively all of Curiosity's data return from the Martian surface. The link from Curiosity to MRO incorporates a number of new features enabled by the Electra and Electra-Lite software-defined radios on MRO and Curiosity, respectively. Specifically, the Curiosity-MRO link has for the first time on Mars relay links utilized frequency-agile operations, data rates up to 2.048 Mb/s, suppressed carrier modulation, and a new Adaptive Data Rate algorithm in which the return link data rate is optimally varied throughout the relay pass based on the actual observed link channel characteristics. In addition to the baseline surface relay support by ODY and MRO, the MEX relay service has been verified in several successful surface relay passes, and MEX now stands ready to provide backup relay support should NASA's orbiters become unavailable for some period of time.

[1]  R. Anderson,et al.  Mars Science Laboratory Mission and Science Investigation , 2012 .

[2]  David Bell,et al.  Chapter 2 The Electra Radio , 2006 .

[3]  R. Thomas,et al.  Mars relay coordination lessons learned , 2005, 2005 IEEE Aerospace Conference.

[4]  Peter Schmitz,et al.  An Interplanetary and Interagency Network - Lander Communications at Mars , 2008 .

[5]  James K. Erickson,et al.  Telecommunications relay support of the Mars Phoenix Lander mission , 2010, 2010 IEEE Aerospace Conference.

[6]  Charles D. Edwards,et al.  A Martian Telecommunications Network: UHF Relay Support of the Mars Exploration Rovers by the Mars Global Surveyor, Mars Odyssey, and Mars Express Orbiters , 2004 .

[7]  Charles D. Edwards Relay communications for Mars exploration , 2007, Int. J. Satell. Commun. Netw..

[8]  Charles D. Edwards,et al.  The Electra proximity link payload for Mars relay telecommunications and navigation , 2003 .

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

[10]  F. Abilleira,et al.  Entry, Descent, and Landing Communications for the 2011 Mars Science Laboratory , 2012 .

[11]  D. Allard,et al.  Mars Relay Operations Service (MaROS): Managing strategic and tactical relay for the evolving Mars network , 2012, 2012 IEEE Aerospace Conference.

[12]  Charles D. Edwards,et al.  Relay communications strategies for Mars exploration through 2020 , 2006 .

[13]  Alan Lee,et al.  The Electra Radio , 2006 .

[14]  Roy E. Gladden Mars Recon naissance Orbiter: The History of Supporting the Phoenix Lander , 2009 .

[15]  Mark D. Garcia,et al.  Entry, Descent, and Landing Communications for the 2007 Phoenix Mars Lander , 2008 .