Voyager spacecraft system. Volume A - Preferred design for flight spacecraft and hardware subsystems, part II Final technical report
Subsystems development in proposed Voyager spacecraft design
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Subsystems development in proposed Voyager spacecraft design
Alternate mission objectives, design characteristics, and system and subsystem designs for Voyager spacecraft system
Operational support equipment needed to support Voyager spacecraft mission
Design for operational support equipment for 1969 test flight, Voyager spacecraft system
Operational support equipment for Voyager flight spacecraft
Solid-liquid systems sized for 1971 and 1973 missions and 1975 and 1977 missions, Apollo lunar excursion module descent propulsion system, and Titan III-C transtage
Telecommunication system requirements and design for Voyager spacecraft 1971
Voyager spacecraft subsystem level requirements in guidance and control, power, propulsion, and engineering mechanics including structures and packaging
Voyager spacecraft construction scheduling and implementation planning - management, logistics, and auditing review
Preferred Voyager spacecraft design rationale - alternate mission objectives and spacecraft designs
Voyager spacecraft trade-off design parameters in telecommunication subsystems and between telecommunication system and other systems - data encoder and data storage systems
Alternate designs for guidance and control, power, controller and sequencer systems for Voyager spacecraft - effect of alternate designs on schedule and implementation
Operational support equipment design for Voyager spacecraft - system test and launch complex equipment
Spacecraft functional description, mission objectives, design characteristics and system requirements of 1969 Voyager test flight
Operational support equipment for 1969 Voyager spacecraft
Mission objectives and systems design criteria for 1971 Voyager spacecraft concept
Functional descriptions of subsystems for 1971 Voyager flight spacecraft
Functional descriptions of Operational Support Equipment /OSE/ for preliminary design of Voyager spacecraft