TY - GEN
T1 - Vibration Testing of Phytec VM-051 Thermal Camera
AU - Sarnoff, Isaac
AU - Kalos, Sebastian
AU - Roberts, Henry
AU - Manenti, Laura
AU - Arneodo, Francesco
N1 - Publisher Copyright:
© 2021 International Astronautical Federation, IAF. All rights reserved.
PY - 2021
Y1 - 2021
N2 - The United Arab Emirates (UAE) will be sending a compact rover to the Moon in 2024. Among many other devices, the rover will be equipped with a thermal camera. In this work we use a modal shaking machine (“the shaker”) to simulate the conditions that the camera must survive during rocket launch. The shaker is programmed to generate sinusoidal accelerations at specified frequencies that mirror those exhibited during rocket launch. To assess for any damage to the camera components, we inspect the camera before and after the test using four different tests, including microscope imaging and 3D CT scan. In my talk I will describe the findings of such tests and show how the Phytec-VM051 Thermal Camera can withstand the accelerations necessary for space flight without detectable structural damage and while maintaining its ability to reliably image temperatures. Finally, I will also outline the prospects for this work such as additional acoustic testing, and applications to other components or missions.
AB - The United Arab Emirates (UAE) will be sending a compact rover to the Moon in 2024. Among many other devices, the rover will be equipped with a thermal camera. In this work we use a modal shaking machine (“the shaker”) to simulate the conditions that the camera must survive during rocket launch. The shaker is programmed to generate sinusoidal accelerations at specified frequencies that mirror those exhibited during rocket launch. To assess for any damage to the camera components, we inspect the camera before and after the test using four different tests, including microscope imaging and 3D CT scan. In my talk I will describe the findings of such tests and show how the Phytec-VM051 Thermal Camera can withstand the accelerations necessary for space flight without detectable structural damage and while maintaining its ability to reliably image temperatures. Finally, I will also outline the prospects for this work such as additional acoustic testing, and applications to other components or missions.
KW - Force Limited Vibration Testing
UR - http://www.scopus.com/inward/record.url?scp=85127456689&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85127456689&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:85127456689
T3 - Proceedings of the International Astronautical Congress, IAC
BT - 54th IAA Symposium on Safety, Quality and Knowledge Management in Space Activities 2021 - Held at the 72nd International Astronautical Congress, IAC 2021
PB - International Astronautical Federation, IAF
T2 - 54th IAA Symposium on Safety, Quality and Knowledge Management in Space Activities 2021 at the 72nd International Astronautical Congress, IAC 2021
Y2 - 25 October 2021 through 29 October 2021
ER -