Progress Report from the Mechanical/Shield Group Feb 19, 2003 * The next meeting is Feb. 26th at 9:30 AM in the Fermilab Cafeteria. * Shield and Cold Plate Engineering and Integration Clark Reid continues to work on importing the SNAP satellite integration model into Ideas. He has produced more 2D drawings of some shielding components. They are on our web page. Sandor Fehers has imported some of the integration model with SolidWorks. We agree we need to have at least one SoldiWorks liscense within our group, as that is the program they are using at LBL. * Shielding Simulation Igor Rakhno and Sergei Striganov showed their progress in importing heavy ion interactions into MARS. They showed the dE/dx(MeV/cm) and range (cm) in 27Al for protons, 4He, 12C, 27Al, and 56Fe as a function of projectile energy. The energy loss calculation is that by EM interaction. Fritz Dejongh is working on the Spenvis simulation. He noted that some satellite shielding simulations use simple "line-of-sight" traces of the material in the satellite in a given direction. He asked if the 3d models can produce these sorts of summaries. TD showed comparisons of relative EM and nuclear-interaction shielding thickness of aluminum, molybdenum, and tungsten. If a cone is 180 kg and is 1 m tall with radius 1/3 m, then the thickness is T. A is atomic number. Z is charge. I is nuclear interaction length. I(cm) ~ 35 (g/cm^2) A^1/3. Material Density (kg/m^3) A Z I(cm) T (cm) ZZT T/I ------------------------------------------------------------------ Aluminum 2740 27 13 39 8 13.5 0.21 Tungsten 1.93e4 184 74 9.6 0.9 49 0.094 Molybdenum 1.03e4 96 42 15 1.7 30 0.11 ZZT (Charge^2 * T) is a crude measure of the effectiveness at shielding from electromagnetic radiation. More is better. T/I is the number of interaction lengths. With this few, it's not clear more interaction lengths is better.