Critical functions of the spacecraft and interactions between the spacecraftand the MOS, Delta II and DSN shall be testable at a level of assembly adequateto verify the function or interface to be tested. Normal and fault protection/correctionhardware and software states and sequences shall be testable at the systemlevel. Spacecraft and test system shall provide for safe ground testingof all hazardous spacecraft commands.
fault tolerant and fault testable hardware design.rar | temp
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