| タイトル | Contemporary Impact Analysis Methodology for Planetary Sample Return Missions |
| 著者（英） | Armand, Sasan C.; Bayandor, Javid; Perino, Scott V.; Samareh, Jamshid A. |
| 発行日 | 2015-06-04 |
| 言語 | eng |
| 内容記述 | Development of an Earth entry vehicle and the methodology created to evaluate the vehicle's impact landing response when returning to Earth is reported. NASA's future Mars Sample Return Mission requires a robust vehicle to return Martian samples back to Earth for analysis. The Earth entry vehicle is a proposed solution to this Mars mission requirement. During Earth reentry, the vehicle slows within the atmosphere and then impacts the ground at its terminal velocity. To protect the Martian samples, a spherical energy absorber called an impact sphere is under development. The impact sphere is composed of hybrid composite and crushable foam elements that endure large plastic deformations during impact and cause a highly nonlinear vehicle response. The developed analysis methodology captures a range of complex structural interactions and much of the failure physics that occurs during impact. Numerical models were created and benchmarked against experimental tests conducted at NASA Langley Research Center. The postimpact structural damage assessment showed close correlation between simulation predictions and experimental results. Acceleration, velocity, displacement, damage modes, and failure mechanisms were all effectively captured. These investigations demonstrate that the Earth entry vehicle has great potential in facilitating future sample return missions. |
| NASA分類 | Astrodynamics |
| レポートNO | NF1676L-18648 |
| 権利 | Copyright |
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