Inflatable solar sails for low-cost robotic Mars missions
Robert Frisbee, John Brophy
- 发表年份
- 1997
- 引用次数
- 5
摘要
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.
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