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Extra resources for A field approach to the description of gravitational interaction
This message contains the following: • Time (in UTC) • Warning flags – Observatory coarse pointing – Observatory fine pointing – Thruster firing – HGA movement – Instrument power service off • SSR partition fill status The STEREO Observatory 31 Likewise, each instrument provides a status message to the spacecraft bus containing the following: • A request to be powered down, by power service • Status of SECCHI recloseable doors (SECCHI only) • Status of HI ontime door (SECCHI only). The spacecraft bus polls the instruments for data via the MIL-STD-1553 bus according to a fixed bus schedule.
13 STEREO RF subsystem block diagram 38 A. Driesman et al. 0703 Emergency, Spacecraft Roll Primary rates are shown in bold their own thermal requirements. Table 7 shows the thermal operational and survival requirements for all observatory bus components and instruments. The thermal isolation requirement that was levied on all components was >20°C/W. In most cases this requirement was met, with a few components falling between 10 and 20°C/W. Heat density requirements also were levied, thus removing the need for active heat transfer.
These southward field regions can occur both in the compressed plasma between the shock and CME and in the CME itself, which often contains magnetic field structures called magnetic clouds. Second, the impact of the CME compresses Earth’s day side magnetosphere, which can leave high altitude geostationary satellites directly exposed to the solar wind. The third way CMEs drive space weather is through the production of SEP events, as discussed in the previous section. Although recent strides have been made in our understanding of the relationship between CMEs and space weather, our current ability to forecast space weather disturbances caused by CMEs is still relatively poor.