Mars 2007 Smart Lander Mission Science Definition Team Report

Status Report From: NASA HQ
Posted: Thursday, October 11, 2001

Note: Full report available in Adobe Acrobat format

Related Document: "Reference Science Scenario for 2007 Mars Smart Lander Mission Science Definition Team (SDT) Report "

1.0 Introduction

The 2007 Mars Smart Lander Mission Science Definition Team (SDT), chartered by NASA Headquarters in April 2001, was given the task of defining and prioritizing the science goals, objectives, investigations, and measurements associated with this landed opportunity. In addition, the SDT was asked to consider: (a) the extent to which meeting science objectives associated with the 2007 mission should depend on precursor measurements such as those expected from the planned Mars Reconnaissance Orbiter (MRO), (b) whether or not direct life detection experiments should be attempted, (c) the extent to which the mission should be used for technology development and testing to help prepare for Mars Sample Return, and (d) the importance of radioisotope power sources (RPS) for meeting mission objectives. For reference, Appendix 1 provides the detailed SDT Charter, Appendix 2 lists SDT Membership, and Appendix 3 is a summary of the tasks that led to generation of this report.

The report is structured in the following way: An overview of the main aspects of the Mars Smart Lander Mission is first presented to set the stage for consideration of science opportunities. Next, specific science objectives are defined that are of highest priority and well matched to the mission objectives. Two options for surface science are then delineated, followed by detailed scenario analyses that demonstrate that the options are credible. The report closes with specific recommendations associated with programmatic issues and a concluding statement.

2.0 Overview of Smart Lander Mission

The Mars 2007 Smart Lander Mission will feature a precision landing capability to get to within approximately 5 km of a given target site. This capability will allow landing in any of a large number of relatively safe places that are in close proximity to rougher areas of very high scientific interest. In addition, a terminal hazard detection and avoidance system will be used to select safe areas within the landing ellipse, thereby allowing a landing to occur in more hazardous terrain than possible before the 2007 opportunity. Touchdown robustness will also be enhanced by judicious hardening of landed systems using appropriate technologies. Landing site altitudes will need to be less than +2.5 km above the MOLA-derived zero elevation of Mars. These capabilities in total will allow delivery of approximately 1620 kg (820 kg for landing systems; 800 kg for surface systems, including approximately 70 to 100 kg of science payload) of landed assets in 2007 with a much wider selection of locations than possible, for example, with the 2003 Mars Exploration Rover (MER) landing system.

Launch, transfer, and arrival constraints associated with the 2007 opportunity, combined with the payload mass, dictate use of a Delta IV or Atlas V launch vehicle and an arrival subsolar longitude of approximately 130 degrees (northern summer). Direct entry will be used to place assets on the surface. For solar-powered systems the range of latitudes for surface operations will be limited to approximately 30 degrees about the equator. The mission lifetime and operational activities will also be highly modulated by seasonal controls on amount of sunlight. On the other hand, use of RPS power systems would allow access to all locations on the planet below the altitude cutoff, with an extended period of operations. A primary mission duration of 180 sols is assumed for solar-powered missions and 360 sols for RPS-powered systems. It is noted that RPS systems could easily provide steady power for up to 720 sols, but that the total cost of the mission would need to increase significantly to accommodate flight systems designed to operate over such a long period of time.

These main characteristics of the Smart Lander Mission were the background for the SDT deliberations. The job of the SDT was to make recommendations focused on science to be accomplished during this landed opportunity and the payloads needed to accomplish the science, and to comment on topics specifically requested in the SDT Charter (Appendix 1). The Smart Lander precision landing, coupled with delivery of a large payload to the surface, offers an opportunity to conduct science on an unprecedented scale on Mars. The SDT looked at this opportunity to define the Smart Lander Mission as the capstone mission for this decade by making groundbreaking scientific discoveries and paving the way for the sample return mission.

3.0 Science Objectives and Measurements Matched to Mission Capabilities

The Mars Exploration Payload Analysis Group (MEPAG) has developed a comprehensive strategic plan for exploration of Mars that is focused on the overarching goals of understanding whether or not life got started and evolved, the causes and timing of current and past climates, and the nature and extent of resources available at and beneath the surface [Greeley, 2000]. The role and availability of water is a central theme. Further, a full understanding of life, climate, and resources requires detailed study of the evolution of the interior, surface, and atmosphere, along with the interplay of various cycles (e.g., climatic and tectonic) that may have dominated Mars during past epochs. All of these results impact our understanding of the extent to which surface and near-surface materials can be used to support human expeditions and the extent to which humans need to cope with hazards during their missions.

The MEPAG document was the starting point for SDT deliberations. That is, the goals, objectives, investigations, and measurements defined by MEPAG were scrutinized for applicability to the Smart Lander Mission, refined and updated as needed, and used to form the backbone of the science to be accomplished during the 2007 landed opportunity. What follows in this section is a discussion of the science objectives that can be addressed for each of the Mars Exploration ProgramÕs main themes, which are: development and evolution of life, current and past climates, evolution of the surface and interior, and preparation for human expeditions.


1.0 Intro 1
2.0 Overview of Smart Lander Mission
3.0 Science Objectives and Measurements Matched to Mission Capabilities
3.1 Development and Evolution of Life
3.2 Current and Past Climates
3.3 Structure and Dynamics of the Interior
3.4 Preparation for Human Exploration and Development of Space
4.0 Mission Options
4.1 Overview
4.2 Mobile Geobiology Explorer
4.3 Multidisciplinary Platform
5.0 Detailed Surface Operations Scenarios
6.0 Programmatic Issues and Recommendations
6.1 Selecting Between the Explorer and the Platform
6.2 Technology Development
6.3 Enhanced Mission Using Radioisotope Power System
6.4 Precursor Measurements
6.5 Planetary Protection
6.6 Facilities, Instruments, and Integrated Packages
6.7 Education and Public Engagement
7.0 Concluding Remarks
8.0 References Cited
9.0 Appendix 1 - Science Definition Team Charter
10.0 Appendix 2 - Science Definition Team Membership
11.0 Appendix 3 - Science Definition Team Activities
12.0 Appendix 4 - Example Payloads
13.0 Appendix 5 Š Detailed Mission Scenarios for Mobile Geobiology Explorer

Note: Full report available in Adobe Acrobat format

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