| タイトル | Advanced Supersonic Parachute Inflation Research Experiment-2 (ASPIRE2) Parachute Modeling and Flight Mechanics Performance |
| 本文(外部サイト) | https://ntrs.nasa.gov/citations/20240014284 |
| 著者(英) | Evan Roelke; Justin S. Green; Soumyo Dutta |
| 著者所属(英) | Analytical Mechanics Associates (United States); Langley Research Center; Langley Research Center |
| 発行日 | 2025-01-27 |
| 抄録 | The Advanced Supersonic Parachute Inflation Research Experiment-2 (ASPIRE2) program is designed to test and qualify the supersonic parachute for the Mars entry, descent, and landing stage of the Mars Sample Return campaign. The ASPIRE2 test was planned for early 2026 and would have involved testing the parachute at deployments of Mach 2.1 and higher load conditions than previous Mars missions. The ASPIRE2 simulation builds upon a previous test framework from the ASPIRE tests in 2017-2018 used to qualify the Mars 2020 parachute, but due to new requirements, the modeling and simulation for ASPIRE2 has needed development and characterization of different sensitivities. This paper looks at the mission design as of
mid-2024 and presents the trade space for qualifying the parachute in a dynamic environment. |
| NASA分類 | Aerodynamics |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/1301877 |