GCR Methods in Radiation Transport F.A. Cucinotta And M.Y. Kim NASA Johnson Space Center.

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Presentation transcript:

GCR Methods in Radiation Transport F.A. Cucinotta And M.Y. Kim NASA Johnson Space Center

Overview CRÈME used in HZETRN and other codes Badhwar and O’Neill Model developed for HZETRN applications in 1993 –Elemental spectra for H, He, C, O, Si, Fe –Crème formula for other elements New version by Pat O’Neill in 2004 fit to ACE and includes LSS spectra –Elemental spectra for all elements Isotopic composition integrated into HZETRN in 2005 using historical data including Ulysses

Isotopic Composition Historical data used to re-distribute Badhwar-O’Neill elemental flux into isotopic fractions Energy-independent

Solar Modulation of GCR Badhwar and O’Neill use self-consistent solution to transport Local Intersteller source (LIS) for each element using Fokker-Plank radial diffusion equation based on Parker (1965) –Neutron monitor counts –Sun-spot number Kim et al. use a statistical model to predict probability distribution for level of future GCR modulation

Sunspot number is well correlated with many observable space quantities and represents variation in the space radiation environment. A solar cycle statistical model (1-3) was developed based on the accumulating cycle sunspot data. A predictive model for GCR radiation environment (4,5) represented by GCR deceleration potential (  ) was derived from GCR flux and ground-based Climax neutron monitor rate measurements over the last four decades.  Prediction of radiation environments and doses for future space exploration missions. Relationship between large SPE occurrence and   A probability of SPE in mission period. Future GCR Modulation- Approach

Population Group of Declining Phase of Cycle 23 (Cumulative Mean Value and Statistical Fluctuation)

Projections of Solar Cycles 23 and 24 A basis for estimating of exposure in future space missions

Climax Neutron Monitor Rate Measurements and Projection to Solar Cycles 23 and 24

GCR Environments and Point Dose Equivalents inside Spacecraft