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1964 Mission Objectives accomplished achievable mis activate redundant elements automatic CC&S closest approach competing characteristics Considerations in Spacecraft decision-making process design approach design concept design conflicts design criteria design of planetary design process encounter sequence engineering as applied examine failure mode effect feedback flyby function requires ground command identify initiate the encounter initiating critical mand Mariner Mars 1964 means of achieving means of initiating ments mission objective achievement Mission Operations Systems mode effect analysis On-board logic operating mode planetary equipment planetary spacecraft design preprogrammed primary mission objective Project Office Proper operation quirements recording sequence required functional capabilities Required Spacecraft System roll attitude control scan spacecraft capability spacecraft design activity spacecraft subsystem Spacecraft System Capability Spacecraft System engineering special functions subsystem functional capabilities subsystem interactions system design activity system designer's responsibilities telemetry television picture television subsystem term system engineering tions total spacecraft trajectory dispersions week after encounter