ESA title
New MEMs Accelerometer
Enabling & Support

New MEMs Accelerometer to Meet Rising Performance Demands

28/09/2022 992 views 5 likes
ESA / Enabling & Support / Space Engineering & Technology / Shaping the Future

Demand for high-performance MEMS accelerometers able to withstand harsh environments is increasing due to their inherent advantages versus legacy technologies and the proliferation of monitoring and control application requiring sensors.

An activity with Safran Colibrys SA, in Switzerland and GSTP Element 1 has developed a closed-loop MEMS accelerometer to meet the requirements of a radiation-hard accelerometer for incorporation in a low-resource standalone three-axis MEMS accelerometer or inertial measurement unit.​

MEMS technology is the ideal solution for the space market, as it addresses the performance requirements while levering significant size, power, cost and robustness.​

The approach was to carry out a pre-study of the suitability of a MEMS closed-loop accelerometer for space applications

The activity re-assessed the space accelerometer requirements for various ESA missions (e.g., ExoMars, MSR, Heracles, Plato) and potential new use cases (e.g., exploration, satellite, mini-satellite, launcher, vehicle). It then validated the radiation tolerance and thermal performance of the closed-loop architecture. Finally, the activity generated a product definition proposal for the realisation of a MEMS closed-loop accelerometer for space.

The proposed SA500 sensor is a single-axis, closed-loop, rad-hard MEMS accelerometer consisting of two modules: A mixed signal board populated with a multichip module (including both MEMS accelerometer die and an analog/mixed-signal front-end ASIC); And a digital board with a radiation-hardened microcontroller.

The activity’s developed sensor is well positioned to meet or exceed the majority of the mission requirements identified in this study, including Entry Descent and Landing (EDL), Rover Navigation, guidance & navigation, monitoring & control and tilt sensing. Only the gravitational and orbit transfer applications, which require niche accelerometers very low full-scale ranges (order of µg), were not suitable for our proposed sensor.

4000133599/20 closed in 2022.

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