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Inflatable solar sails for low-cost robotic Mars missions

Robert Frisbee, John Brophy

Year
1997
Citations
5

Abstract

This paper presents an evaluation of the use of solar sails based on inflatable-structures technologies to perform low-cost robotic planetary missions. We show that there is a significant potential synergism between the emerging technologies of microspacecraft and inflatable solar sails that offer the unique capability of performing planetary science missions using a small, low-cost launch vehicle, such as the Pegasus XL, with a launch cost of less than $25M. In the example evaluated here, a roughly 100-m diameter inflatable solar sail can deliver a 48-kg microspacecraft payload to Mars orbit with a trip time of about 725 days. Once in orbit, the microspacecraft can perform orbit changes (including atmospheric entry) with no expenditure of propellant by using the solar sail.

Keywords

InflatableMars Exploration ProgramAerospace engineeringSolar sailAstrobiologyMarine engineeringAeronauticsExploration of MarsComputer scienceEnvironmental science

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