1. Radiation testing of a commercial 6-axis MEMS inertial navigation unit at ENEA Frascati proton linear accelerator
- Author
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F. Cardelli, L. Piersanti, Emiliano Trinca, Marco Sabatini, F. Fortini, Vincenzo Surrenti, Giovanni B. Palmerini, Monia Vadrucci, G. Bazzano, Paolo Nenzi, Luigi Picardi, Concetta Ronsivalle, A. Ampollini, Bazzano, G., Ampollini, A., Cardelli, F., Fortini, F., Nenzi, P., Palmerini, G. B., Picardi, L., Piersanti, L., Ronsivalle, C., Surrenti, V., Trinca, E., Vadrucci, M., and Sabatini, M.
- Subjects
Atmospheric Science ,010504 meteorology & atmospheric sciences ,Computer science ,COTS ,Aerospace Engineering ,radiation hardness ,01 natural sciences ,Linear particle accelerator ,law.invention ,law ,Inertial measurement unit ,0103 physical sciences ,Aerospace engineering ,010303 astronomy & astrophysics ,Radiation hardening ,Inertial navigation system ,0105 earth and related environmental sciences ,business.industry ,Navigation system ,Astronomy and Astrophysics ,Particle accelerator ,Gyroscope ,IMU ,MEMS ,Geophysics ,Space and Planetary Science ,Absorbed dose ,proton ,General Earth and Planetary Sciences ,business - Abstract
We present the first results of a novel collaboration activity between ENEA Frascati Particle Accelerator Laboratory and University La Sapienza Guidance and Navigation Laboratory in the field of Radiation Hardness Assurance (RHA) for space applications. The aim of this research is twofold: (a) demonstrating the possibility to use the TOP-IMPLART proton accelerator for radiation hardness assurance testing, developing ad hoc dosimetric and operational procedures for RHA irradiations; (b) investigating system level radiation testing strategies for Commercial Off The Shelf (COTS) components of interest for SmallSats space missions, with focus on devices and sensors of interest for guidance, navigation and control, through simultaneous exploration of Total Ionizing Dose (TID), Displacement Damage (DD) dose and Single-Event Effects (SEE) with proton beams. A commercial 6-axis integrated Micro Electro-Mechanical Systems (MEMS) inertial navigation system (accelerometer, gyroscope) was selected as first Device Under Test (DUT). The results of experimental tests aimed to define an operational procedure and the characterization of radiation effects on the component are reported, highlighting the consequence of the device performance degradation in terms of the overall navigation system accuracy. Doses up to 50 krad(Si) were probed and cross sections for Single-Event Functional Interrupt (SEFI) evaluated at a proton energy of 30 MeV.
- Published
- 2021