Drube, Line and Harris, Alan and Weisenberger, Steffen and Engel, K. and Falke, A. and Delchambre, Simon and Ziegler, Tobias and Eggl, S. (2017) NEOTωIST: A relatively Inexpensive Kinetic Impactor Demonstration Mission Concept. Planetary Defence Conference 2017, 2017-05-15 - 2017-05-19, Tokyo, Japan.
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Abstract
Mission concept: NEOTωIST stands for Near-Earth Object Transfer of angular momentum (ω∙I) Spin Test, and is a concept for a kinetic impactor demonstration mission, which aims to change the spin rate of an asteroid by impacting it off-center (Drube et al. 2016, Engel et al. 2016). The change would be measured by means of lightcurve measurements with Earth-based telescopes. In contrast to most other kinetic impactor demonstration mission concepts, NEOTωIST does not require a reconnaissance spacecraft to rendezvous with the target asteroid for orbit change and impact-effect measurements, and is therefore a relatively inexpensive alternative. The NEOTωIST mission would determine the efficiency of momentum transfer (the β-factor) during an impact, and help mature the technology required for a kinetic impactor mission, both of which are important precursor measures for a future space mission to deflect an asteroid by collisional means in an emergency impact hazard situation.
| Item URL in elib: | https://elib.dlr.de/111694/ | ||||||||||||||||||||||||||||||||||||
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| Document Type: | Conference or Workshop Item (Speech) | ||||||||||||||||||||||||||||||||||||
| Title: | NEOTωIST: A relatively Inexpensive Kinetic Impactor Demonstration Mission Concept | ||||||||||||||||||||||||||||||||||||
| Authors: |
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| Date: | 2017 | ||||||||||||||||||||||||||||||||||||
| Refereed publication: | No | ||||||||||||||||||||||||||||||||||||
| Open Access: | Yes | ||||||||||||||||||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||||||||||||||||||
| In SCOPUS: | No | ||||||||||||||||||||||||||||||||||||
| In ISI Web of Science: | No | ||||||||||||||||||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||||||||||||||||||
| Keywords: | etic impactor, beta-factor, mission design | ||||||||||||||||||||||||||||||||||||
| Event Title: | Planetary Defence Conference 2017 | ||||||||||||||||||||||||||||||||||||
| Event Location: | Tokyo, Japan | ||||||||||||||||||||||||||||||||||||
| Event Type: | international Conference | ||||||||||||||||||||||||||||||||||||
| Event Start Date: | 15 May 2017 | ||||||||||||||||||||||||||||||||||||
| Event End Date: | 19 May 2017 | ||||||||||||||||||||||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||||||||||||||||||||
| HGF - Program: | Space | ||||||||||||||||||||||||||||||||||||
| HGF - Program Themes: | Space Exploration | ||||||||||||||||||||||||||||||||||||
| DLR - Research area: | Raumfahrt | ||||||||||||||||||||||||||||||||||||
| DLR - Program: | R EW - Space Exploration | ||||||||||||||||||||||||||||||||||||
| DLR - Research theme (Project): | R - Vorhaben Planetary Evolution and Life (old) | ||||||||||||||||||||||||||||||||||||
| Location: | Berlin-Adlershof | ||||||||||||||||||||||||||||||||||||
| Institutes and Institutions: | Institute of Planetary Research > Leitungsbereich PF | ||||||||||||||||||||||||||||||||||||
| Deposited By: | Drube, Line | ||||||||||||||||||||||||||||||||||||
| Deposited On: | 20 Jul 2017 14:27 | ||||||||||||||||||||||||||||||||||||
| Last Modified: | 24 Apr 2024 20:16 |
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