Book contents
- Frontmatter
- Contents
- Preface
- Acknowledgements
- List of acronyms and abbreviations
- PART I Engineering issues specific to entry probes, landers or penetrators
- PART II Previous atmosphere/surface vehicles and their payloads
- PART III Case studies
- 21 Surveyor landers
- 22 Galileo probe
- 23 Huygens
- 24 Mars Pathfinder and Sojourner
- 25 Deep Space 2 Mars Microprobes
- 26 Rosetta lander Philae
- 27 Mars Exploration Rovers: Spirit and Opportunity
- Appendix Some key parameters for bodies in the Solar System
- Bibliography
- References
- Index
27 - Mars Exploration Rovers: Spirit and Opportunity
Published online by Cambridge University Press: 12 August 2009
- Frontmatter
- Contents
- Preface
- Acknowledgements
- List of acronyms and abbreviations
- PART I Engineering issues specific to entry probes, landers or penetrators
- PART II Previous atmosphere/surface vehicles and their payloads
- PART III Case studies
- 21 Surveyor landers
- 22 Galileo probe
- 23 Huygens
- 24 Mars Pathfinder and Sojourner
- 25 Deep Space 2 Mars Microprobes
- 26 Rosetta lander Philae
- 27 Mars Exploration Rovers: Spirit and Opportunity
- Appendix Some key parameters for bodies in the Solar System
- Bibliography
- References
- Index
Summary
Following the success of the Mars Pathfinder project in 1997, there was a resurgence of interest in the deployment of an untethered rover on the surface of Mars. The concept of a semi-autonomous and freely roving vehicle was mooted as a follow-on to the Viking missions of the late 1970s. Almost twenty years were to pass before a rover was to be operated on Mars. After the Mars Pathfinder mission, NASA had proposed to send a rover equipped with a geology/chemistry payload, dubbed the ‘Athena’ suite, to Mars in 2001. Various constraints led to the redesign of the mission for a 2003 launch, although experiments of the payload were carried on the ill-fated Mars Polar Lander. In 2000 the Mars Exploration Rover mission was selected, with a launch-date flight three years later. This time, the Athena payload was to be duplicated, carried on two identical 174 kg rovers. Designated MER-A and MER-B, the spacecraft carrying the rovers were launched to Mars on separate Delta 2 boosters, making use of the favourable 2003 window for low-energy trajectories. The rovers on each craft were targeted to different regions of Mars. The MER-A craft, carrying the ‘Spirit’ rover, arrived on 4 January 2004 and was directed toward Gusev crater (14.5°S, 175.5°E) in the Aeolis region of Mars. This crater is the terminus of the fluid-cut Ma'adim Vallis, and Gusev was thought to host geological clues to the presence of water on Mars.
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- Planetary Landers and Entry Probes , pp. 304 - 312Publisher: Cambridge University PressPrint publication year: 2007