Development of a miniature atomic accelerometer for spacecraft drag-free force measurement
ORAL
Abstract
Atom interferometers demonstrate state-of-the-art performance in inertial sensors. This technology can be used as an onboard three-axis absolute accelerometer in spacecraft for planetary science measurements. Such an instrument would allow us to measure non-gravitational forces on spacecraft such as atmospheric drag and solar radiation in order to obtain drag-free measurements, opening new possibilities for exploring diverse planetary environments.
Our instrument is designed to meet the constraints of a deep space planetary orbiter mission, with a low size, weight and power consumption, while reaching a sensitivity of 3×10-8 m/s2/√Hz with a sequential measurement of 3 Hz per axis to match the expected state-of-the-art radio link precision. To achieve this, the atomic vacuum chamber is made of a single block of titanium with brazed sapphire windows, which is fully sealed under ultra-high vacuum without active pump. The atomic physical package will be of 2 L and 2 kg. The laser is designed to be agile and compact with a fully fibred laser and optics system and expected to fit in a 1 L and 1 kg package. We also discuss the microgravity environment requirements and schemes for lifting the velocity degeneracy. We will describe the design concept and progresses toward realization of the atomic device.
Our instrument is designed to meet the constraints of a deep space planetary orbiter mission, with a low size, weight and power consumption, while reaching a sensitivity of 3×10-8 m/s2/√Hz with a sequential measurement of 3 Hz per axis to match the expected state-of-the-art radio link precision. To achieve this, the atomic vacuum chamber is made of a single block of titanium with brazed sapphire windows, which is fully sealed under ultra-high vacuum without active pump. The atomic physical package will be of 2 L and 2 kg. The laser is designed to be agile and compact with a fully fibred laser and optics system and expected to fit in a 1 L and 1 kg package. We also discuss the microgravity environment requirements and schemes for lifting the velocity degeneracy. We will describe the design concept and progresses toward realization of the atomic device.
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Presenters
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Mehdi Langlois
Jet Propulsion Laboratory
Authors
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Mehdi Langlois
Jet Propulsion Laboratory
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Saesun Kim
Jet Propulsion Laboratory
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Yun-Jhih Chen
Jet Propulsion Laboratory
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Sheng-Wey Chiow
Jet Propulsion Laboratory
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Nan Yu
Jet Propulsion Laboratory, Je Propulsion Laboratory