PRE2024 3 Group13: Difference between revisions
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[3] https://doi.org/10.1007/s11434-010-4198-9 | [3] https://doi.org/10.1007/s11434-010-4198-9 | ||
[4] https://doi.org/10.1007/s11433-011-4561-0 | [4] https://doi.org/10.1007/s11433-011-4561-0 | ||
[5] https://doi.org/10.1006/icar.2000.6545 | |||
[6] https://doi.org/10.1016/j.icarus.2009.11.034 | |||
[7] https://doi.org/10.1006/icar.2000.6545 | |||
Summary: | Summary: | ||
From [1] it was found that He-3 is implanted into the lunar surface by the solar wind. The problem is not the implantation, however, but the retention of the He-3 within the lunar surface. The retention of He-3 depends on the grain size of the lunar regolith [1] (<50 micron seems to hold the most helium-3), the electroconductivity of the lunar regolith (TiO2 was mentioned)[3] and it also seems to depend on the solar exposure [2], meaning less sunlight is better able to retain the He-3. This would mean that craters at the lunar poles seem to be the best option [2]. | From [1] it was found that He-3 is implanted into the lunar surface by the solar wind. The problem is not the implantation, however, but the retention of the He-3 within the lunar surface. The retention of He-3 depends on the grain size of the lunar regolith [1] (<50 micron seems to hold the most helium-3), the electroconductivity of the lunar regolith (TiO2 was mentioned)[3] and it also seems to depend on the solar exposure [2], meaning less sunlight is better able to retain the He-3. This would mean that craters at the lunar poles seem to be the best option [2]. The Chang-E-1 mission was able to measure the thickness of the regolith layer by measuring the thermal radiation of the lunar regolith [4][5][6] (I don't fully understand this yet). Another method was found in [7] by using radar waves (at 70cm) and measuring the thickness by using scattering from the underlying substrate. | ||
Thomas: | Thomas: | ||
Revision as of 17:50, 13 February 2025
Ideas
- we can also use swarm behavior of ants, krill, termite, locusts, bees.
- maybe we can distinguish between a few mother robots that controls the other robots, like in a ant nest: Queen, worker, male (to fertilize the queen), Warriors .etc
Users: Space Agencies (ESA, NASA, etc.)
Group members
| Name | Student ID | Email address |
|---|---|---|
| Bas Coppus | 1706160 | b.coppus@student.tue.nl |
| Mikolaj Pujanek | 1732595 | m.p.pujanek@student.tue.nl |
| Maksim Fisekovic | 1889524 | m.fisekovic@student.tue.nl |
| Ingmar Verweij | 1629433 | i.verweij@student.tue.nl |
| Thomas Passon | 1890190 | t.passon@student.tue.nl |
Introduction
Type an introduction
Who does what
Bas: transporting Helium back to Earth
Mikolaj: bringing Helium to refinery/mass driver
Maksim: control of the swarm
Ingmar: locating Helium
Thomas: mining Helium
Literature review
Bas:
Mikolaj:
Maksim:
Ingmar: [1] http://www.lpi.usra.edu/meetings/lpsc2007/pdf/2175.pdf [2] https://doi.org/10.1016%2Fj.icarus.2009.12.032 [3] https://doi.org/10.1007/s11434-010-4198-9 [4] https://doi.org/10.1007/s11433-011-4561-0 [5] https://doi.org/10.1006/icar.2000.6545 [6] https://doi.org/10.1016/j.icarus.2009.11.034 [7] https://doi.org/10.1006/icar.2000.6545
Summary: From [1] it was found that He-3 is implanted into the lunar surface by the solar wind. The problem is not the implantation, however, but the retention of the He-3 within the lunar surface. The retention of He-3 depends on the grain size of the lunar regolith [1] (<50 micron seems to hold the most helium-3), the electroconductivity of the lunar regolith (TiO2 was mentioned)[3] and it also seems to depend on the solar exposure [2], meaning less sunlight is better able to retain the He-3. This would mean that craters at the lunar poles seem to be the best option [2]. The Chang-E-1 mission was able to measure the thickness of the regolith layer by measuring the thermal radiation of the lunar regolith [4][5][6] (I don't fully understand this yet). Another method was found in [7] by using radar waves (at 70cm) and measuring the thickness by using scattering from the underlying substrate.
Thomas:
Individual effort
| Name | Total time | Progress and time |
|---|---|---|
| Bas Coppus | 4h | Making small basic sections in the wiki page and trying to understand how to edit the page works (1h). Finding a subject to research and how to implement this research into a program, prototype or a literature research and finding some papers (2h) . Meeting at 12-02-2025 (1h) |
| Mikolaj Pujanek | ||
| Maksim Fisekovic | ||
| Ingmar Verweij | Find a research subject (1h), Wednesday meeting (1hr), Literature review (4hrs) | |
| Thomas Passon |
| Name | Total time | Progress and time |
|---|---|---|
| Bas Coppus | ||
| Mikolaj Pujanek | ||
| Maksim Fisekovic | ||
| Ingmar Verweij | ||
| Thomas Passon |
| Name | Total time | Progress and time |
|---|---|---|
| Bas Coppus | ||
| Mikolaj Pujanek | ||
| Maksim Fisekovic | ||
| Ingmar Verweij | ||
| Thomas Passon |
| Name | Total time | Progress and time |
|---|---|---|
| Bas Coppus | ||
| Mikolaj Pujanek | ||
| Maksim Fisekovic | ||
| Ingmar Verweij | ||
| Thomas Passon |
| Name | Total time | Progress and time |
|---|---|---|
| Bas Coppus | ||
| Mikolaj Pujanek | ||
| Maksim Fisekovic | ||
| Ingmar Verweij | ||
| Thomas Passon |
| Name | Total time | Progress and time |
|---|---|---|
| Bas Coppus | ||
| Mikolaj Pujanek | ||
| Maksim Fisekovic | ||
| Ingmar Verweij | ||
| Thomas Passon |
| Name | Total time | Progress and time |
|---|---|---|
| Bas Coppus | ||
| Mikolaj Pujanek | ||
| Maksim Fisekovic | ||
| Ingmar Verweij | ||
| Thomas Passon |
Sources
- ↑ Ehresmann, M., Gabrielli, R. A., Herdrich, G., & Laufer, R. (2017). Lunar based massdriver applications. Acta Astronautica, 134, 189–196. https://doi.org/10.1016/j.actaastro.2017.02.007