Most of the C&DH hardware is located in the main bus structure of the SOM. It is an integrated C&DH subsystem which controls and monitors the entire spacecraft. The WISP has a separate C&DH subsystem. Table 9 summarizes the system.
Architecture | Integrated; Bus |
On-Board Computer | 3.05 MIPS, 24 megabits of memory |
Recorder | 2 1-Gigabit solid-state recorders |
WISP Architecture | Single Unit Point-to-Point |