Application of gyrocompassing to space missions Final technical report
Gyrocompassing with sensors or inertial platforms for use on planetary surface or in free orbital flight
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Gyrocompassing with sensors or inertial platforms for use on planetary surface or in free orbital flight
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
Design concepts, management philosophy and program highlights of research toward Voyager spacecraft development
Spacecraft design for Voyager mission
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 1969 test flight options and spacecraft configurations, and two launch vehicles - Voyager project
Design for operational support equipment for 1969 test flight, Voyager spacecraft system
Management tasks associated with preparation and implementation of spacecraft system design, development, launch, and mission support for Voyager project
Scientific investigation of solar system with instrumented, unmanned spacecraft to fly, orbit and land on planets - Voyager project
Hardware subsystems for flight spacecraft, design reliability, interface control, and mission objectives - Voyager project
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