Mars Exploration News  
Detailing The Science Of Man on Mars


Washington DC (SPX) Jun 14, 2005
The Mars Human Precursor Science Steering Group was chartered by MEPAG in June 2004 to analyze the priorities for precursor investigations, measurements, and technology/infrastructure demonstrations that would have a significant effect on the cost and risk of the first human mission to Mars.

Based on this analysis, the MHP SSG proposes the following revised phrasing for MEPAG's Goal IV, Objective A, and within it the investigations that follow (in priority order).

The measurements needed to carry out these investigations are described in the subsequent sections of this white paper.

All of the measurements listed below, which are listed in priority order by the degree of impact on risk reduction, would have value to planning the human exploration of Mars (and most particularly the first human mission to the martian surface, for which our lack of knowledge will be greatest).

However, the authors of this report are not in a position to determine how much risk needs to be removed in order for the first human mission to be judged acceptably safe.

Thus, we cannot a priori determine how many of these measurements need to be successfully completed (i.e. required) before the first human mission can fly.

Obviously, a larger precursor program will reduce the risk more than a smaller precursor program. However, the decision on safety thresholds must be deferred to others.

Recommended revision to MEPAG Objective IVA.

Objective A. Obtain knowledge of Mars sufficient to design and implement a human mission with acceptable cost, risk and performance.

The following four investigations are of indistinguishable high priority.

1A. Characterize the particulates that could be transported to mission surfaces through the air (including both natural aeolian dust and particulates that could be raised from the martian regolith by ground operations), and that could affect hardware's engineering properties. Analytic fidelity sufficient to establish credible engineering simulation labs and/or performance prediction/design codes on Earth is required.

1B. Determine the variations of atmospheric dynamical parameters from ground to >90 km that affect EDL and TAO including both ambient conditions and dust storms.

1C. Determine if each martian site to be visited by humans is free, to within acceptable risk standards, of replicating biohazards which may have adverse effects on humans and other terrestrial species. Sampling into the subsurface for this investigation must extend to the maximum depth to which the human mission may come into contact with uncontained martian material.

1D. Characterize potential sources of water to support ISRU for eventual human missions. At this time it is not known where human exploration of Mars may occur. However, if ISRU is determined to be required for reasons of mission affordability and/or safety, then, therefore the following measurements for water with respect to ISRU usage on a future human mission may become necessary (these options cannot be prioritized without applying constraints from mission system engineering, ISRU process engineering, and geological potential):

The following investigations are listed in descending priority order.

2. Determine the possible toxic effects of martian dust on humans.

3. Derive the basic measurements of atmospheric electricity that affects TAO and human occupation.

4. Determine the processes by which terrestrial microbial life, or its remains, is dispersed and/or destroyed on Mars (including within ISRU-related water deposits), the rates and scale of these processes, and the potential impact on future scientific investigations.

5. Characterize in detail the ionizing radiation environment at the martian surface, distinguishing contributions from the energetic charged particles that penetrate the atmosphere, secondary neutrons produced in the atmosphere, and secondary charged particles and neutrons produced in the regolith.

6. Determine traction/cohesion in martian soil/regolith (with emphasis on trafficability hazards, such as dust pockets and dunes) throughout planned landing sites; where possible, feed findings into surface asset design requirements.

7. Determine the meteorological properties of dust storms at ground level that affect human occupation and EVA.

This is the executive summary of the report issued by the Mars Human Precursor Science Steering Group. The complete PDF file is available for downloading here.

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