| タイトル | Supersonic Retropropulsion Technology Development in NASA's Entry, Descent, and Landing Project |
| 本文（外部サイト） | http://hdl.handle.net/2060/20120014589 |
| 著者（英） | Post, Ethan A.; Korzun, Ashley; Kelb, Bil; Rhode, Matthew N.; Zarchi, Kerry A.; Edquist, Karl T.; Dyakonov, Artem A.; Berry, Scott A.; Schauerhamer, Daniel G. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2012-06-18 |
| 言語 | eng |
| 内容記述 | NASA's Entry, Descent, and Landing (EDL) space technology roadmap calls for new technologies to achieve human exploration of Mars in the coming decades [1]. One of those technologies, termed Supersonic Retropropulsion (SRP), involves initiation of propulsive deceleration at supersonic Mach numbers. The potential benefits afforded by SRP to improve payload mass and landing precision make the technology attractive for future EDL missions. NASA's EDL project spent two years advancing the technological maturity of SRP for Mars exploration [2-15]. This paper summarizes the technical accomplishments from the project and highlights challenges and recommendations for future SRP technology development programs. These challenges include: developing sufficiently large SRP engines for use on human-scale entry systems; testing and computationally modelling complex and unsteady SRP fluid dynamics; understanding the effects of SRP on entry vehicle stability and controllability; and demonstrating sub-scale SRP entry systems in Earth's atmosphere. |
| NASA分類 | Spacecraft Propulsion and Power |
| レポートNO | NF1676L-15052 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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