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Engineering project - Design of the Support Structure for the Sun Sensors, Deployable Magnetometer and Optical Camera of EventSat

Institut
Lehrstuhl für Spacecraft Systems (TUM-ED)
Typ
Bachelorarbeit /
Inhalt
experimentell / konstruktiv /  
Beschreibung

Engineering Project: Support Structure for the EventSat Sensors and Camera

Chair of Spacecraft Systems, TUM | Start: ASAP | 2 months, approx. 150 hours (concentrated)

EventSat is a 6U CubeSat under development at the Chair of Spacecraft Systems, heading to a Sun-synchronous orbit in 2027. We are looking for a student to design, manufacture and integrate the support structure for the satellite's two sun sensors, its deployable magnetometer and a small optical camera.

The structure has to meet competing constraints:

  • clear fields of view for the sun sensors;
  • magnetic cleanliness for the magnetometer;
  • a Sun-safe line of sight for the camera;
  • the limits of the Exolaunch deployer and the 6U structure.

You will take the part from requirements to hardware:

  • derive the requirements;
  • develop the design in CAD;
  • verify it with finite element analysis;
  • release it to manufacturing;
  • mount it on EventSat with the real sensors and camera, checking every interface.

What you get: hands-on work on a satellite that will fly, as part of the EventSat ADCS and structure teams.

What we expect:

  • working knowledge of CAD and FEA;
  • availability of about 18-20 hours per week over the two months;
  • an independent, systematic way of working.

Contact: Vincenzo Messina (vincenzo.messina<script>document.write('@');</script>

<noscript>(at)</noscript>tum.de), Francesco Salmaso (francesco.salmaso<script>document.write('@');</script><noscript>(at)</noscript>tum.de)
Voraussetzungen

• Working knowledge of CAD and FEA is required, given the compressed schedule

Möglicher Beginn
sofort
Kontakt
Vincenzo Messina
Tel.: +49 89 289 55752
vincenzo.messinatum.de
Ausschreibung