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Journal of Vacuum Science & Technology A Vacuum Surfaces and Films

Design and qualification of an UHV system for operation on sounding rockets

Jens Große, Stephan Seidel, Dennis Becker, Maike Diana Lachmann, Marco Scharringhausen, Claus Braxmaier, Ernst Maria Rasel

Published May 1, 2016• 16 citations
Publisher

Abstract

The sounding rocket mission MAIUS-1 has the objective to create the first Bose–Einstein condensate in space; therefore, its scientific payload is a complete cold atom experiment built to be launched on a VSB-30 sounding rocket. An essential part of the setup is an ultrahigh vacuum system needed in order to sufficiently suppress interactions of the cooled atoms with the residual background gas. Contrary to vacuum systems on missions aboard satellites or the international space station, the required vacuum environment has to be reached within 47 s after motor burn-out. This paper contains a detailed description of the MAIUS-1 vacuum system, as well as a description of its qualification process for the operation under vibrational loads of up to 8.1 gRMS (where RMS is root mean square). Even though a pressure rise dependent on the level of vibration was observed, the design presented herein is capable of regaining a pressure of below 5 × 10−10 mbar in less than 40 s when tested at 5.4 gRMS. To the authors' best knowledge, it is the first UHV system qualified for operation on a sounding rocket.

DOI
10.1116/1.4947583

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The sounding rocket mission MAIUS-1 has the objective to create the first Bose–Einstein condensate in space; therefore, its scientific payload is a complete cold atom experiment built to be launched on a VSB-30 sounding rocket. An essential part of the setup is an ultrahigh vacuum system needed in order to sufficiently suppress interactions of the cooled atoms with the residual background gas. Contrary to vacuum systems on missions aboard satellites or the international space station, the required vacuum environment has to be reached within 47 s after motor burn-out. This paper contains a detailed description of the MAIUS-1 vacuum system, as well as a description of its qualification process for the operation under vibrational loads of up to 8.1 gRMS (where RMS is root mean square). Even though a pressure rise dependent on the level of vibration was observed, the design presented herein is capable of regaining a pressure of below 5 × 10−10 mbar in less than 40 s when tested at 5.4 gRMS. To the authors' best knowledge, it is the first UHV system qualified for operation on a sounding rocket.
During the two sounding rocket missions MAIUS-2 and MAIUS-3, it is planned to perform sequential and simultaneous dualspecies atom interferometry with Bose-Einstein condensates of Potassium-41 and Rubidium-87. The scientific payload of the MAIUS missions will be launched on-board a VSB-30 sounding rocket launched from Esrange in Sweden. The flights of these rockets allows for approximately 360 s of microgravity conditions. The microgravity environment offers experiments on timescales that are not possible on ground based experiments. To perform long lifetimes of the BEC, a pressure <= 5·10^(-10) mbar needs to be reached and maintained in the vacuum chamber. During ascent of the rocket, vibrational loads of 1.8 g RMS in the frequency range of 20-2000 Hz and accelerations of up to 13 g are applied to the vacuum system and the payload. During re-entry and landing static loads can reach a level of up to 50 g. The ultra-high vacuum system presented in this talk is designed to withstand these loads while maintaining the vacuum quality. Therefore, the sealing technologies and pumping concepts which are used under this challenging requirements, needed to be tested and qualified. This talk presents the ultra-high vacuum system of the MAIUS-2/3 payload in detail, as well as its vibration and qualification tests at the shaker test facility at the Center of Applied Space Technology and Microgravity (ZARM) in Bremen.
The MAIUS-1 experiment is a pathfinder quantum optics experiment about to fly on a VSB-30 sounding rocket in November 2015. The scientific objective of the mission is to demonstrate the feasibility of creating a Bose-Einstein Condensate and performing atom interferometry aboard a sounding rocket with Rubidium 87atoms. This paper will summarize the thermal and mechanical design of the payload and its (sub)systems. Moreover the qualification procedures and the results of the qualification test will be presented.
In January 2017 a first sounding rocket mission housing experiments on matter-wave interferometry, MAIUS-1 (Materiewellen-Interferometrie unter Schwerelosigkeit Matter-Wave Interferometry under Microgravity), has been launched. Following this campaign, two sounding rocket missions, MAIUS-2 and MAIUS-3, are planned to perform sequential and simultaneous dual-species atom interferometry with Bose-Einstein condensates (BEC) of Potassium-41 and Rubidium-87. The scientific payload of the MAIUS missions will be launched on-board a VSB-30 sounding rocket launched from Esrange in Sweden. The ights of these rockets allows for approximately 360 s of microgravity conditions. It therefore overs a microgravity environment for experiments on timescales not accessible in ground based experiments, such as in the drop tower. During ascent of the rocket, vibrational loads of up to 1.8 g RMS in the frequency range of 20- 2000 Hz and accelerations of up to 13 g can occur. Furthermore, static loads, caused by the re-entry and the landing, can be as high as 50 g. Both missions MAIUS-2 and MAIUS-3 y the same payload, called MAIUS-B. Consequently, the payload needs to be designed to withstand the aforementioned loads
The QUANTUS consortium started activities to perform atom interferometry on a sounding rocket in the year 2011. Three sounding rocket missions (MAIUS-1 to MAIUS-3) have been planned to demonstrate BoseEinstein condensation and atom interferometry with rubidium and potassium atoms. Two different payloads MAIUS-A and MAIUS-B have been designed qualified and integrated in the time frame from 2011 until 2020. The MAIUS-A scientific payload is capable of performing single species experiment with rubidium only and was used as a technology demonstrator in the MAIUS-1 mission. The MAIUS-1 mission was conducted in fall 2016. On the 23rd of January 2017 the payload MAIUS-A was launched on a VSB-30 sounding rocket. The payload created the first Bose-Einstein condensate (BEC) and performed atom interferometry aboard a sounding rocket with rubidium 87 atoms [Becker 2018]. Its successor MAIUS-B will be able to perform simultaneous experiments with Bose-Einstein Condensates of Rubidium-87 and Potassium-41 atoms. In order to achieve this ambitious scientific goal the experiments use various sensitive instruments imposing strong requirements on the thermal and mechanical design of the scientific payload. This paper gives a summary of the MAIUS-A and MAIUS-B scientific payload design with a focus on the thermal control system. Furthermore, the design of the GSE and the water cooling umbilicals is presented. The paper closes with an outlook on future atom interferometry payloads on sounding rockets and beyond.
The QUANTUS consortium started activities to perform atom interferometry on a sounding rocket in the year 2011. Three sounding rocket missions (MAIUS-1 to 3) have been planned to demonstrate Bose-Einstein condensation and atom interferometry with rubidium and potassium atoms. Two different payloads MAIUS-A and MAIUS-B are being designed, qualified and integrated in the time frame from 2011 until 2020. The MAIUS-A scientific payload demonstrated the first Bose-Einstein Condensates in Space in the challenging environment aboard a two-staged VSB-30 sounding rocket on the 23rd of January 2017. In order to achieve this ambitious scientific goal the experiment used various sensitive instruments imposing strong requirements on the thermal and mechanical design of the scientific payload. This paper gives a summary of the MAIUS-A and MAIUS-B scientific payload design. Furthermore, the lessons learned from the MAIUS-1 maiden flight as well as the integration and testing activities and their impact on the MAIUS-B scientific payload design are presented. The paper closes with an outlook on future atom interferometry payloads on sounding rockets and beyond.
Cooling atoms to Nano-Kelvin requires an ultra-high vacuum system with complex features, such as coated optical accesses, paramagnetic materials, or differential pumping stages. Furthermore, the sensitivity of atom interferometers, one promising application of ultra-cold atoms, scales with the free evolution time (T) of the cold ensembles. In order to increase T, microgravity becomes necessary. Hence, the development of reliable, miniaturized UHV systems with the capability to withstand the rough environment of microgravity platforms is a key task to pave the way for high performance cold atom instruments. In order to minimize such complex vacuum systems various tests have to be performed. For instance the measurement of outgassing rates for critical components inside the chamber and leakage rates of metal sealed windows allow a more detailed dimensioning of the vacuum pumps. In addition to the challenge of miniaturization, most of the microgravity platforms are linked to a rough thermal and mechanical environment. Vacuum pumps and seals are supposed to endure vibrations and loads of rocket launches or drop tower impacts. In the case of the sounding rocket mission MAIUS, the motors induced loads to the payload of up to 13 g. This talk presents the challenges for vacuum systems on microgravity platforms. Test beds for outgassing rate measurement, window sealing technologies and loaded CF flanges are shown and first results for the tests are given