A compact and robust diode laser system for atom interferometry on a sounding rocket

被引:63
|
作者
Schkolnik, V. [1 ,5 ]
Hellmig, O. [3 ]
Wenzlawski, A. [2 ]
Grosse, J. [4 ,6 ]
Kohfeldt, A. [5 ]
Doeringshoff, K. [1 ]
Wicht, A. [1 ,5 ]
Windpassinger, P. [2 ]
Sengstock, K. [3 ]
Braxmaier, C. [4 ,6 ]
Krutzik, M. [1 ]
Peters, A. [1 ,5 ]
机构
[1] Humboldt Univ, Inst Phys, Newtonstr 15, D-12489 Berlin, Germany
[2] Johannes Gutenberg Univ Mainz, Inst Phys, D-55099 Mainz, Germany
[3] Univ Hamburg, Inst Laserphys, Luruper Chaussee 149, D-22761 Hamburg, Germany
[4] Univ Bremen, ZARM, D-28359 Bremen, Germany
[5] Leibniz Inst Hochstfrequenztech, Ferdinand Braun Inst, Gustav Kirchhoff Str 4, D-12489 Berlin, Germany
[6] Deutsch Zentrum Luft & Raumfahrt eV DLR, Inst Raumfahrtsyst, Robert Hooke Str 7, D-28359 Bremen, Germany
来源
APPLIED PHYSICS B-LASERS AND OPTICS | 2016年 / 122卷 / 08期
关键词
QUANTUM GAS EXPERIMENTS; GRAVITY GRADIOMETER; SPACE;
D O I
10.1007/s00340-016-6490-0
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
We present a diode laser system optimized for laser cooling and atom interferometry with ultra-cold rubidium atoms aboard sounding rockets as an important milestone toward space-borne quantum sensors. Design, assembly and qualification of the system, combing micro-integrated distributed feedback (DFB) diode laser modules and free space optical bench technology, is presented in the context of the MAIUS (Matter-wave Interferometry in Microgravity) mission. This laser system, with a volume of 21 l and total mass of 27 kg, passed all qualification tests for operation on sounding rockets and is currently used in the integrated MAIUS flight system producing Bose-Einstein condensates and performing atom interferometry based on Bragg diffraction. The MAIUS payload is being prepared for launch in fall 2016. We further report on a reference laser system, comprising a rubidium stabilized DFB laser, which was operated successfully on the TEXUS 51 mission in April 2015. The system demonstrated a high level of technological maturity by remaining frequency stabilized throughout the mission including the rocket's boost phase.
引用
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页数:8
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