Voyager capsule phase B. Volume IV - Entry science package. Part E - Alternatives and systems analysis. Part F - Future mission options Final report
Design alternatives and systems analysis of Voyager entry science package for Mars atmosphere probe
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Design alternatives and systems analysis of Voyager entry science package for Mars atmosphere probe
Major equipment and subsystem descriptions of Voyager entry science package for Mars
Reliability, planetary quarantine, support equipment, and interface alternatives of Voyager entry science package for Mars atmosphere probe
Voyager capsule surface laboratory system - design concepts and objectives
Voyager capsule surface laboratory system - mission analysis, system functional requirements, and design selection and alternatives
Voyager capsule surface laboratory system - subsystem design analysis
Voyager capsule surface laboratory system - subsystem design analysis
Voyager capsule surface laboratory system - subsystem functional descriptions
Voyager capsule surface laboratory system - subsystem functional descriptions
Voyager capsule surface laboratory system - operational support equipment
Voyager capsule surface laboratory system - reliability
Propulsion system selection considerations for Voyager spacecraft including Minuteman solid with liquid restartable midcourse, orbit trim system, LEM descent stage and transtage
System design of Voyager-class Mars Probe/ Lander, considering selections of entry aeroshell, landed capsule and descent and postimpact instrumentation
Scientist role in automated laboratory for remote biological exploration of planets
Mars landing guidance requirements for unmanned lander after separation from interplanetary flyby space vehicle
Voyager thermal insulation requirements noting tests of vapor deposited Au on Mylar and Kapton
Systems analysis and engineering, operational support and mission-dependent equipment, and spacecraft definition for Voyager Mars project
A comprehensive study to develop software to simulate the dynamic operation of water reclamation systems in long-term closed-loop life support systems is being carried out as part of an overall program for the design of systems for a moon station or a Mars voyage. This project is being done in parallel with a similar effort in the Department of Chemistry to develop durable accurate low-cost sensors for monitoring of trace chemical and biological species in recycled water supplies. Aspen-Plus software is being used on a group of high-performance work stations to develop the steady state descriptions for a number of existing technologies. Following completion, a dynamic simulation package will be developed for determining the response of such systems to changes in the metabolic needs of the crew and to upsets in system hardware performance.