Table 3.
ICME signatures observed at different spacecraft.
| ICME | MO | MC | MC-like | Vsw | Bmax |
 |
Vsw | FR | |||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| s/c | Tstart | Tend | Tstart | Tend | Tstart | Tend | Tstart | Tend | ICME | MO | type | ||
| (DOY in 2013) | (km s−1) | (nT) | (km s−1) | ||||||||||
| (1) | (2) | (3) | (4) | (5) | (6) | (7) | (8) | (9) | (10) | (11) | (12) | (13) | (14) |
| MESS | 232.53 | 233.32 | 232.79 | 233.32 | 232.79 | 233.00 | 233.11 | 233.32 | 800a | 168.9 | 28.8 | 575a | NES |
| STB | 234.09 | 235.29 | 234.54 | 234.89 | 234.54 | 234.75 | – | – | 600 | 9.2 | 10.0 | 568 | WSE |
| STA | 234.29 | 236.98 | 234.97 | 236.98 | 235.02 | 236.05 | 236.17 | 236.98 | 455 | 16.6 | 16.6 | 398 | ESW |
Notes. Column 1: observing spacecraft. Columns 2–9: start and end of the ICME, MO, MC, and MC-like structures, respectively. Column 10: mean solar wind speed within the ICME. Columns 11–13: maximum magnetic field strength, scaled magnetic field strength to the heliocentric distance of STEREO-A (details given in the main text), and mean solar wind speed within the MO, respectively. Column 14: type of field rotation (e.g. Bothmer & Schwenn 1998) determined by eye. a MESSENGER mean speed taken from the ENLIL simulation (Sect. 5.2 in Paper I).
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