Title :
A deterministic electron, photon, proton and heavy ion radiation transport suite for the study of the Jovian system
Author :
Norman, Ryan B. ; Badavi, Francis F. ; Blattnig, Steve R. ; Atwell, William
Author_Institution :
NASA Postdoctoral Program Fellow, NASA Langley Res. Center, Hampton, VA, USA
Abstract :
A deterministic suite of radiation transport codes, developed at NASA Langley Research Center (LaRC), which describe the transport of electrons, photons, protons, and heavy ions in condensed media is used to simulate exposures from spectral distributions typical of electrons, protons and carbon-oxygen-sulfur (C-O-S) trapped heavy ions in the Jovian radiation environment. The particle transport suite consists of a coupled electron and photon deterministic transport algorithm (CEPTRN) and a coupled light particle and heavy ion deterministic transport algorithm (HZETRN). The primary purpose for the development of the transport suite is to provide a means for the spacecraft design community to rapidly perform numerous repetitive calculations essential for electron, proton and heavy ion radiation exposure assessments in complex space structures. In this paper, the radiation environment of the Galilean satellite Europa is used as a representative boundary condition to show the capabilities of the transport suite. While the transport suite can directly access the output electron spectra of the Jovian environment as generated by the Jet Propulsion Laboratory (JPL) Galileo Interim Radiation Electron (GIRE) model of 2003; for the sake of relevance to the upcoming Europa Jupiter System Mission (EJSM), the 105 days at Europa mission fluence energy spectra provided by JPL is used to produce the corresponding dose-depth curve in silicon behind an aluminum shield of 100 mils ( 0.7 g/cm2). The transport suite can also accept ray-traced thickness files from a computer-aided design (CAD) package and calculate the total ionizing dose (TID) at a specific target point. In that regard, using a low-fidelity CAD model of the Galileo probe, the transport suite was verified by comparing with Monte Carlo (MC) simulations for orbits JOI-J35 of the Galileo extended mission (1996-2001). For the upcoming EJSM mission with a potential launch date of 2020, the transport suite is used to compute the traditional aluminum-silicon dose-depth calculation as a standard shieldtarget combination output, as well as the shielding response of high charge (Z) shields such as tantalum (Ta). Finally, a shield optimization algorithm is used to guide the instrument designer with the choice of graded-Z shield analysis.
Keywords :
Jupiter; aerospace instrumentation; astronomical techniques; planetary atmospheres; radiation effects; radiation protection; space vehicles; AD 1996 to 2001; Europa Jupiter System Mission; Europa mission fluence energy spectra; Galileo Interim Radiation Electron model; JOI-J35 orbit; Jet Propulsion Laboratory; Jovian radiation environment; Monte Carlo simulations; NASA Langley Research Center; aluminum-silicon dose-depth calculation; carbon-oxygen-sulfur trapped heavy ions; computer-aided design; coupled electron-and-photon deterministic transport algorithm; deterministic suite; dose-depth curve; electron spectra; electron transports; graded-Z shield analysis; heavy ion deterministic transport algorithm; high charge shields; photon transports; proton transports; radiation transport codes; ray-traced thickness files; shield optimization algorithm; spectral distributions; total ionizing dose; Electron traps; Instruments; Jupiter; Materials; Orbits; Protons; Solid modeling;
Conference_Titel :
Aerospace Conference, 2011 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4244-7350-2
DOI :
10.1109/AERO.2011.5747247