Astrix 1120
Overview
Astrix 1000 provides the satellite AOCS with a three-axis measurement of the rotation with a very high reliability level, adapted to 15 years GEO mission in continuous operation. One compact box implements three gyros oriented on the three faces of a corner cube, and their relevant electronics. The use of 2 Astrix 1000 offers very simple and reliable redundancy architecture.
It is proposed as an option with 3 additional accelerometers as a full navigation capability, for deep space missions. Designed to operate within the radiation worst case environment, compatible with the environment of 15 years lifetime GEO Telecom missions. The EEE, opto-electronics and opto components are fully compliant to HiRel Telecom satellite standard (ECSS-QST-60 C class 1 or equivalent).
One compact box implements three gyros oriented on the three faces of a corner cube, and their relevant electronics. The use of 2 Astrix 1000 offers a very simple and reliable redundancy architecture.
Optional accelerometers can be added to provide a full navigation capability for deep space missions. The EEE, opto-electronics and opto components are fully compliant to HiRel Telecom satellite standard (ECSS-Q-ST-60C class 1 or equivalent).
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Overview
- Name
- Astrix 1120
- Vendor
- Airbus
- Subsystem
- ACDS Subsystem
- Component Type
- IMU/IRU
- Form Factor
- SmallSat
- Heritage
- Yes
Vendor Details
- Name
- Airbus
- Website
- https://www.airbus.com/
- Founded
- 1970
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Specifications
- Subsystem
- ACDS Subsystem
- Component Type
- IMU/IRU
- Form Factor
- SmallSat
- Vendor
- Airbus
- Dry Mass
- 4.5 kg
- Average Power
- 13.5 W
- Heritage
- Yes
- Status
- In Production
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