A Space weather information service based upon remote and in-situ measurements of coronal mass ejections heading for Earth - A concept mission consisting of six spacecraft in a heliocentric orbit at 0.72 AU | Journal of Space Weather and Space Climate

Satellite mission concepts developed at the Alpbach 2013 Summer School on space weather

Open Access

Fig. 3.

Total ionizing dose in silicon versus aluminum absorber thickness inside solid aluminum spheres calculated with SPENVIS. The blue lines indicate the required limit of 10 krad corresponding to a shielding thickness of 9 mm aluminum.

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