DOI | Resolve DOI: https://doi.org/10.2514/6.2015-2112 |
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Author | Search for: Underwood, John C.; Search for: Saundersy, Arrun; Search for: Rogersy, Steven B.; Search for: Lingardz, J. Stephen; Search for: Marraffa, Lionel; Search for: Ferracina, Luca; Search for: Larose, Guy L.1; Search for: McTavish, Sean A. M.1 |
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Affiliation | - National Research Council of Canada. Aerospace
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Format | Text, Article |
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Conference | 23rd AIAA Aerodynamic Decelerator Systems Technology Conference, 2015, 30 March 2015 through 2 April 2015, Daytona Beach, Florida |
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Physical description | 9 p. |
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Subject | drops; martian surface analysis; parachutes; Wind stress; drop test; European Space Agency; low altitudes; Mars missions; parachute design; subsonic wind tunnels; wind tunnel tests; wind tunnels |
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Abstract | A wind tunnel test campaign has been carried out to investigate the performance of seven parachute types as part of a European Space Agency programme researching potential subsonic parachutes for future Mars missions. The overall programme also includes high altitude sub-scale drop tests and low altitude, full-scale drop tests of some of the parachute designs. The results of the wind tunnel test campaign are presented and the data for the different designs of parachute are compared.. © 2015, AIAA American Institute of Aeronautics and Astronautics. All rights reserved. |
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Publication date | 2015-04-02 |
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Publisher | American Institute of Aeronautics and Astronautics |
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In | |
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Language | English |
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Peer reviewed | Yes |
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NPARC number | 21277081 |
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Export citation | Export as RIS |
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Report a correction | Report a correction (opens in a new tab) |
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Record identifier | 1445cf0d-428d-4d7f-8660-aa03db70c54a |
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Record created | 2015-11-23 |
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Record modified | 2020-04-22 |
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