FM design at PDR
Enabling & Support

European IMU Breadboard

22/05/2017 703 views 5 likes
ESA / Enabling & Support / Space Engineering & Technology / Shaping the Future
 Programme:  TRP Workplan,  Achieved TRL:  5
 Reference:  T905-014EC  Closure:  2016
 Contractor(s):  Astrium (FR), SEA (GB)

An IMU, consisting of 3 gyro axes and 3 accelerometer axes, is a critical technology to enable future exploration missions during cruise, aerobraking, entry, descent and landing. No European IMU products are currently available on the market. The exploration mission scenarios require a high accuracy and low mass equipment.

The objectives of the activity are to perform a preliminary unit design, to build and test a breadboard, to fly a demonstrator on the MASER13 sounding rocket, and to produce a development plan for a flight model.

Flight demonstrator
Flight demonstrator

Achievements and status
Within the activity, trade-offs and a preliminary design of an FM were done, based on the heritage 90mm fibre-optic gyro (FOG) and on the ESA-funded SA0120 MEMS accelerometer. A prototype including 3 functional accelerometer channels and electronics has been demonstrated on the MASER13 sounding rocket. Detailed performance tests were done on various hardware breadboards de-risk further development.

A European IMU is a critical sensor for planetary landing missions, and can furthermore be applied to launcher navigation, as well as spacecraft delta-v monitoring during delta-V maneuvers and planetary fly-bys.

Next steps
Maturation of the accelerometer components; Engineering Model (EM) design, manufacturing and testing; recurring cost reduction (e.g. COTS components).


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