Project Dragonfly: A feasibility study of interstellar travel using laser-powered light sail propulsion
Autor: | Lukas Schrenk, Johannes Gutsmiedl, Martin Losekamm, Nikolaos Perakis, Artur Koop |
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Rok vydání: | 2016 |
Předmět: |
020301 aerospace & aeronautics
Engineering Spacecraft business.industry Payload Aerospace Engineering 02 engineering and technology Propulsion 01 natural sciences Interstellar travel Acceleration 0203 mechanical engineering 0103 physical sciences Alpha Centauri Aerospace engineering business Interplanetary spaceflight 010303 astronomy & astrophysics Interstellar probe |
Zdroj: | Acta Astronautica. 129:316-324 |
ISSN: | 0094-5765 |
DOI: | 10.1016/j.actaastro.2016.09.030 |
Popis: | Light sail-based propulsion systems are a candidate technology for interplanetary and interstellar missions due to their flexibility and the fact that no fuel has to be carried along. In 2014, the Initiative for Interstellar Studies (i4is) hosted the Project Dragonfly Design Competition, which aimed at assessing the feasibility of sending an interstellar probe propelled by a laser-powered light sail to another star system. We analyzed and designed a mission to the Alpha Centauri system, with the objective to carry out science operations at the destination. Based on a comprehensive evaluation of currently available technologies and possible locations, we selected a lunar architecture for the laser system. It combines the advantages of surface- and space-based systems, as it requires no station keeping and suffers no atmospheric losses. We chose a graphene-based sandwich material for the light sail because of its low density. Deceleration of the spacecraft sufficient for science operations at the target system is achieved using both magnetic and electric sails. Applying these assumptions in a simulation leads to the conclusion that 250 kg of scientific payload can be sent to Alpha Centauri within the Project Dragonfly Design Competition's constraints of 100 year travel duration and 100 GW laser beam power. This is only sufficient to fulfill parts of the identified scientific objectives, and therefore renders the usefulness of such a mission questionable. A better sail material or higher laser power would improve the acceleration behavior, an increase in the mission time would allow for larger spacecraft masses. |
Databáze: | OpenAIRE |
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