Earth-Moon-Mars Radiation Environment Model N. A. Schwadron, K. Kozarev, L. Townsend, M. Desai, M. A. Dayeh, F. Cucinotta, D. Hassler, H. Spence, M. Pourars,

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Earth-Moon-Mars Radiation Environment Model N. A. Schwadron, K. Kozarev, L. Townsend, M. Desai, M. A. Dayeh, F. Cucinotta, D. Hassler, H. Spence, M. Pourars, E. Wilson, K. Korreck, X. Ao, G. Zank

Space Weather, Safeguarding the Journey Space weather impacts on robotic and human productivity Radiation bombardment on the lunar surface and subsurface

Accomplishments Radiation Biology –Risk models –Radiation Transport Interplanetary Space Earth, Moon, Mars EPREM –Transport Particle Acceleration –Particle radiation throughout inner helioshere –Earth, Moon, Mars EPREM-MHD –Transport Effects –Particle Acceleration Validation –Marie –CRaTER Extended Solar Minimum EMMREM Special Section (Spaceweather Journal; currently, 12 papers)

Select EMMREM Special Section Papers Schwadron et al., EMMREM Framework,Spaceweather Journal, 8, 2010 Schwadron et al., GCR Hazard in the extended solar minimum between cycles 23 and 24, Spaceweather Journal, 8, 2010 PourArsalan et al., Time-dependent estimates of organ dose and dose equivalent rates for human crews in deep space from the 26 Oct 2003 solar energetic particle event (Halloween event) using EMMREM, Space Weather 8, 2010 Townsend et al., Parameterization of LET for the CRaTER Instrument, Spacweather, 8, 2010 Kozarev et al., Modeling the 2003 Halloween Events with EMMREM: Energetic Particles, Radial Gradients and Coupling to MHD, Spaceweather, 8, 2010 Cucinotta et al., Space Radiation Risk Limits and Earth-Moon-Mars Environmental Models, Spaceweather, 8, 2010 Zeitlin, C., et al., Mars Odyssey measurements of GCRs and solar particles in Mars orbit, Spaceweather, 8, 2010 Dayeh, et al, Modeling proton intensity gradients and radiation dose in the inner heliosphere using EMMREM: May 2003 events, Spaceweather, 8, 2010

EMMREM has proved very successful at predicting SEP spectra and radiation dose estimates at different distances in the inner heliosphere. Figures below show two recent papers by which SEP time profiles, onset, and radiation estimates were successfully predicted at Mars (Odyssey) and Ulysses located at 1.44 AU and 4.91 AU, respectively. 1 AU measurement from ACE, SoHO, and GOES. Dayeh, M. A., et al, Space Weather, 8, S00E07, doi: /2009SW Zeitlin, C., et al., Space Weather, 8, S00E06, doi: /2009SW

EMMREM-MHD Coupling – Shock Acceleration from Seed Populations Kozarev et al., Fall AGU, 2010

Modeling Large SEP Events with PATH Code Zank et al., AGU, 2010

Simulation of Earth-Moon-Mars Radiation Environments for Assessments of Radiation Doses Kim et al., AGU, 2010

CRaTER Validation

Long-term GCR Extrapolation

U. Tennessee – EMMREM Accomplishments NNX07AC14G – L. Townsend Lead development of Scenario and Transport code modules Provided capability, in near-real- time, to calculate radiation doses and LET spectra for tissue and electronics behind spacecraft aluminum shields using “looping” BRYNTRN code Provided database of human organ radiation exposures for Al shielding thicknesses relevant to vehicle and habitat designs anywhere in free space or in Mars atmosphere for GCR and SEP spectra covering the entire solar cycle Calculations of doses, dose equivalents and effective dose for GCR and SEP protons at aircraft altitudes in Earth’s atmosphere are completed. Heavy ion component calculations are in progress Publications (author/coauthor) - 10 journal articles - 4 invited paper presentations - 15 contributed paper presentations 3 graduate students supported

Transition to Prediction & Operations New ESMD/LRO Predictive Model Task DescriptionValue to ESMD (1) SEP Prediction Development Uses CRaTER observations and existing models to improve advanced warning of solar proton events (2) Radiation Environment Forecasting Develops analysis and modeling tool combined with CRaTER observations to extend prediction of the radiation environment well beyond low Earth orbit, not only at Moon but also throughout the inner heliosphere, including at Earth, Moon, Mars, Asteroids, and Comets

Next Steps for EMMREM Transition to Operations and Predictive Models Development of Comprehensive Risk Models Coupling between MHD & EPREM Continued development of PATH into a predictive model