Voyager spacecraft. Volume IV - Alternate designs, systems considerations - Appendices Study report, phase IA
Voyager spacecraft subsystem reliability, star and Mars approach sensors, microelectronics, trajectory and orbit, and communications limits
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Voyager spacecraft subsystem reliability, star and Mars approach sensors, microelectronics, trajectory and orbit, and communications limits
Telecommunication, propulsion, control, electric, and mechanical subsystems design for Voyager spacecraft
Stability and control, telecommunication system, solar array design, propellant feed system, and infrared model of Mars for Voyager project
Operational ground support equipment for Voyager project, including data handling system, launch complex equipment, system test complex, and mission dependent equipment
Voyager spacecraft and operation support equipment design and program planning for flight test mission
Voyager spacecraft preferred design
Preferred design for Voyager spacecraft subsystems
Voyager spacecraft implementation plan
Operational support equipment for Voyager spacecraft
Tradeoff analyses for Voyager spacecraft propulsion system selection
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
Systems analysis study relating to applicability of several types of propulsion systems for Voyager missions
Earth-lunar horizon sensor program, design characteristics, and application of horizon sensors to Apollo extension system space missions
Response time and design requirements of earth- lunar horizon sensor program
Synthesis and characterization of vinylaromatic polymers
Elimination of rocket motor ignition by electrostatic initiation through development of electrically insensitive igniter and nonelectric stimulus transfer system