Details
| Originalsprache | Englisch |
|---|---|
| Titel des Sammelwerks | 66th International Astronautical Congress 2015, IAC 2015 |
| Untertitel | Space - The Gateway for Mankind's Future |
| Herausgeber (Verlag) | International Astronautical Federation, IAF |
| Seiten | 627-633 |
| Seitenumfang | 7 |
| ISBN (elektronisch) | 9781510818934 |
| Publikationsstatus | Veröffentlicht - 2015 |
| Veranstaltung | 66th International Astronautical Congress 2015: Space - The Gateway for Mankind's Future, IAC 2015 - Jerusalem, Israel Dauer: 12 Okt. 2015 → 16 Okt. 2015 |
Publikationsreihe
| Name | Proceedings of the International Astronautical Congress, IAC |
|---|---|
| Band | 1 |
| ISSN (Print) | 0074-1795 |
Abstract
The MAIUS-1 experiment is a high precision quantum optics experiment about to fly on a VSB30 sounding rocket in spring 2016. To perform the quantum optics experiments a vacuum chamber with a pressure below 5E-10 mbar is essential. This pressure has to be reached 45 s after motor burn-out. The detailed design and the components of the MAIUS vacuum system will be presented in this paper. This design and the used components have been qualified for operation under vibrational loads of up 8.1 g RMS. A pressure rise has been observed in all test runs, which is caused by temporary leaks at the seals. It was proven that the pressure rise is depending on the level of vibrations applied. The design presented herein is capable of regaining a pressure of 5E-10 mbar in less than 40 s when tested at 5.4 g RMS.
ASJC Scopus Sachgebiete
- Ingenieurwesen (insg.)
- Luft- und Raumfahrttechnik
- Physik und Astronomie (insg.)
- Astronomie und Astrophysik
- Erdkunde und Planetologie (insg.)
- Astronomie und Planetologie
Zitieren
- Standard
- Harvard
- Apa
- Vancouver
- BibTex
- RIS
66th International Astronautical Congress 2015, IAC 2015: Space - The Gateway for Mankind's Future. International Astronautical Federation, IAF, 2015. S. 627-633 (Proceedings of the International Astronautical Congress, IAC; Band 1).
Publikation: Beitrag in Buch/Bericht/Sammelwerk/Konferenzband › Aufsatz in Konferenzband › Forschung › Peer-Review
}
TY - GEN
T1 - Design and qualification of a xuhv system for the use on a sounding rocket Payload
AU - Grosse, Jens
AU - Seidel, Stephan Tobias
AU - Scharringhausen, Marco
AU - Rasel, Ernst Maria
N1 - Funding information: The QUANTUS project is a collaboration of LU Hannover, HU Berlin, U Hamburg, U Ulm, TU Darmstadt, FBH Berlin, U Birmingham, DLR RY Bremen and ZARM at U Bremen. It is supported by the German Space Agency DLR with funds provided by the Federal Ministry of Economics and Technology (BMWi) under grant number DLR 50WM 1131-1137
PY - 2015
Y1 - 2015
N2 - The MAIUS-1 experiment is a high precision quantum optics experiment about to fly on a VSB30 sounding rocket in spring 2016. To perform the quantum optics experiments a vacuum chamber with a pressure below 5E-10 mbar is essential. This pressure has to be reached 45 s after motor burn-out. The detailed design and the components of the MAIUS vacuum system will be presented in this paper. This design and the used components have been qualified for operation under vibrational loads of up 8.1 g RMS. A pressure rise has been observed in all test runs, which is caused by temporary leaks at the seals. It was proven that the pressure rise is depending on the level of vibrations applied. The design presented herein is capable of regaining a pressure of 5E-10 mbar in less than 40 s when tested at 5.4 g RMS.
AB - The MAIUS-1 experiment is a high precision quantum optics experiment about to fly on a VSB30 sounding rocket in spring 2016. To perform the quantum optics experiments a vacuum chamber with a pressure below 5E-10 mbar is essential. This pressure has to be reached 45 s after motor burn-out. The detailed design and the components of the MAIUS vacuum system will be presented in this paper. This design and the used components have been qualified for operation under vibrational loads of up 8.1 g RMS. A pressure rise has been observed in all test runs, which is caused by temporary leaks at the seals. It was proven that the pressure rise is depending on the level of vibrations applied. The design presented herein is capable of regaining a pressure of 5E-10 mbar in less than 40 s when tested at 5.4 g RMS.
UR - http://www.scopus.com/inward/record.url?scp=84991434325&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84991434325
T3 - Proceedings of the International Astronautical Congress, IAC
SP - 627
EP - 633
BT - 66th International Astronautical Congress 2015, IAC 2015
PB - International Astronautical Federation, IAF
T2 - 66th International Astronautical Congress 2015: Space - The Gateway for Mankind's Future, IAC 2015
Y2 - 12 October 2015 through 16 October 2015
ER -